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 62861U 26145.22567823 +.00000000 +00000-0 +42502-3 0 00005
2 62861 53.1607 134.4275 0001421 86.6729 273.4434 15.30210562 01
| Epoch (UTC): | 25 May 2026 05:24:58 |
| Eccentricity: | 0.0001421 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 134.4275° |
| argument of perigee: | 86.6729° |
| revolutions per day: | 15.30210562 |
| mean anomaly at epoch: | 273.4434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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