View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62020U 26145.62662324 +.00000000 +00000-0 +21735-2 0 00002
2 62020 53.1574 21.6479 0001375 181.4190 178.6824 15.69843117 07
| Epoch (UTC): | 25 May 2026 15:02:20 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.1574° |
| perigee height: | 358 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 21.6479° |
| argument of perigee: | 181.4190° |
| revolutions per day: | 15.69843117 |
| mean anomaly at epoch: | 178.6824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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