1. The short answer: the only orbit that hovers is a circle around the equator
A satellite that seems to hover is called a geostationary satellite ("geo" means Earth, "stationary" means not moving). Himawari is one. So are many TV and weather satellites. To seem to hover, a satellite has to do two things at once. It has to circle the Earth in the same time the Earth takes to turn once, and it has to circle in the same direction, west to east [2].
The second thing is where the equator comes in. Treating gravity as pulling a satellite toward the middle of the Earth, the middle of its circular path has to be the middle of the Earth. Of all the circles that fit that rule, only one stays above a single spot on the ground as the Earth turns: the one directly above the equator. This is an explanation from physics rather than a sentence quoted from a source, so the next sections check it step by step.
A quick word on Japan's side of the story. Himawari-9, the satellite doing the day-to-day work, sits at about 140.7° east longitude (that is the same line of longitude that runs through eastern Japan) but at 0° latitude, which is the equator. So Japan is not underneath it. Japan is far to its north, and the satellite looks at Japan at a slant, from the south [1].
2. A hovering satellite is not standing still. It is racing around at the Earth's own pace
The European Space Agency (ESA) gives the numbers. A geostationary satellite is 35,786 kilometers above the equator, and one trip around takes 23 hours 56 minutes and 4 seconds. It travels at about 3 kilometers per second [2].
Why 23 hours 56 minutes and not 24 hours? A day on the clock is measured against the Sun. The Earth turns once relative to the distant stars slightly faster, in about 23 hours 56 minutes, because the Earth also moves along its path around the Sun during the day. A satellite only needs to match the turn relative to the stars, and that is what the ESA figure does.
You can check the speed yourself. The satellite is 35,786 km above the surface, and the Earth's equator has a radius of about 6,378 km, so the satellite is about 42,164 km from the center of the Earth. A circle with that radius is about 2 × 3.14 × 42,164 ≈ 265,000 km long. Dividing by 86,164 seconds (23 h 56 min 4 s) gives about 3.07 km per second, which matches ESA's "about 3 km per second". That path is more than six times the distance around the equator (about 40,000 km), covered in a day.
So why does it look still? Imagine a friend running beside you at exactly your pace. Neither of you is standing still, but your friend never moves in your view. A geostationary satellite and the ground below it are in the same situation.
3. Why a satellite can't hover above Japan: gravity pulls toward the middle of the Earth
Here is the key idea. Gravity is what bends a satellite's path into a circle, and to a good approximation gravity pulls toward the Earth's center. Because of that, the plane of an orbit (the flat sheet that contains the circle) must pass through the center of the Earth.
Now try to hover above a city in the northern half of the world, say at 35° north. To keep above that city, the satellite would have to trace the same small circle the city traces as the Earth turns. That small circle is a line of latitude. It sits north of the equator, and its middle point is on the Earth's axis, not at the Earth's center. Gravity pulls toward the center, not toward that point on the axis, so no orbit can follow it. A simple way to picture it is a rubber band stretched around a ball: it can only slide around a circle that goes through the ball's center, so it can sit around the equator, but it cannot stay around a line of latitude.
What if you tilt the orbit so it does pass through the center? Then the satellite drifts north and south of the equator as it goes around, and it does not stay above the city. The only orbit that goes through the Earth's center and also turns the same way as the Earth, so that it stays on one line of longitude, is the one in the equator's plane.
The writer Arthur C. Clarke put the idea into print in 1945. In a magazine article he noted that an orbit with a radius of 42,000 km has a period of exactly 24 hours (a round number, as we saw above), and that a body in such an orbit, if its plane coincided with the plane of the Earth's equator, would revolve with the Earth [3]. He wrote that this was a plan for radio relays, not a built satellite.
4. What happens if the orbit is tilted? Syncom 2 drew a figure eight in the sky
Real life gives an example. Syncom 2, launched by the United States in July 1963, was the first satellite to orbit once a day with the Earth. According to NASA's records as summarized by reference sites, its orbit was tilted about 33 degrees from the equator, so it was not truly stationary. Reference-site summaries say it swung north and south of the equator, which is what a tilted orbit would do, and describe the track as a figure eight over the Atlantic and Brazil. I could not confirm the exact shape or range in NASA's own records [4].
That fits the idea above. Matching the Earth's turning time is not enough by itself. The orbit must also lie in the equator's plane. Satellites that only match the time are called geosynchronous. Satellites that also sit in the equator's plane are geostationary. A tilted satellite swings north and south even though its timing is right. (The exact shape of the path depends on the orbit, and "a figure eight" is the shape reported for Syncom 2.)
5. What the equator spot made possible: steady views and TV across the Pacific
In his 1945 article, Clarke wrote that for a world service three such stations would be required [3], and ESA today says that just three evenly spaced geostationary satellites can give near-global coverage [2].
The first satellite to reach a true equatorial position was Syncom 3, launched in August 1964 and placed above the Pacific, close to the International Date Line. It is reported to have been used to relay 1964 Tokyo Olympics pictures across the Pacific to television viewers in the United States [4]. Sources I could read describe this as a relay for American viewers, not for the whole Games.
For weather forecasting, the payoff is a steady view. Japan's Meteorological Agency says a geostationary satellite sees about one third of the Earth's surface and always looks at the same region, so it can keep watching storms and fronts that last for days [5].
6. The price of the equator spot: the far north and south are hard to see
From above the equator, places near the poles are seen at a very shallow angle. You can work out where the view ends. The orbit radius is about 42,164 km and the Earth's radius is about 6,378 km. The ratio 6,378 ÷ 42,164 is about 0.151, and the latitude whose cosine is 0.151 is about 81°. This is my own geometry, not a number from the sources: it says that beyond roughly 81° north or south, the ground is hidden behind the curve of the Earth. Well before that, the ground is seen so slantwise that it is stretched and squashed in pictures.
Japan's Meteorological Satellite Center says that high-latitude regions (60° and beyond) are hard to observe from geostationary orbit, and that polar-orbiting weather satellites cover them often. The U.S. NOAA satellites it describes fly at about 850 km and circle the Earth in about 100 minutes, passing near the poles [5]. They see a thin strip (about 3,000 km wide) in sharper detail, while the equator satellites see a huge area all the time. Each kind of satellite does the job the other one cannot.
7. Try it yourself: see why the edge of a ball looks squashed
Draw two circles of the same size on a ball (a rubber ball or an orange will do): one near the middle and one near the top. Hold the ball a short way from your eyes. The middle circle looks round. The top one looks squashed. A satellite above the equator sees the far north in the same way.
If you want to go further, look at a weather satellite image online and compare a region in the middle of the picture with one at the very edge. To read the sources, Clarke's 1945 article is short and is available in English at the link below [3].
Sources
Position and orbit numbers come from Japan's Meteorological Agency (JMA) and ESA. Clarke's quotes come from the reprint of his 1945 article. The 81°, 265,000 km, and 3.07 km/s figures are my own calculations from the ESA numbers. The Syncom details (tilt, figure eight, Olympics relay) were not checked on NASA's own catalogue pages, which would not load for me, so they rest on reference-site summaries and should be read as reported.
- Japan Meteorological Agency, "About meteorological satellite observation" (Japanese page): https://www.jma-net.go.jp/sat_info/himawari/satellite.html (read in full: position about 140.7°E over the equator, about 35,800 km; Himawari-9 in operation)
- European Space Agency, "Types of orbits": https://www.esa.int/Enabling_Support/Space_Transportation/Types_of_orbits (geostationary section read: 35,786 km, 23 h 56 min 4 s, about 3 km/s, three satellites for near-global coverage)
- Arthur C. Clarke, "Extra-Terrestrial Relays," Wireless World, October 1945 (online reprint): https://lakdiva.org.lk/clarke/1945ww/1945ww_oct_305-308.html (passages on the 42,000 km orbit, the equatorial plane, and three stations were read)
- "Syncom," Wikipedia: https://en.wikipedia.org/wiki/Syncom; with NASA NSSDC records for Syncom 2 and 3, 1963-031A and 1964-047A (Wikipedia read in part: Syncom 2 first geosynchronous, Syncom 3 first geostationary. The NASA pages did not load; the tilt, figure eight, dates and Olympics relay come from search-result summaries of them and several reference sites, so they are stated as reported)
- Japan Meteorological Satellite Center, "Geostationary and polar-orbiting meteorological satellites" (Japanese page): https://www.data.jma.go.jp/mscweb/ja/general/geopolar.html (read in full: about one third of the Earth's surface in view, NOAA polar orbiters at about 850 km and 100 minutes, high latitudes above 60°)
Update history
- : First published.