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 62081U 26145.63185792 +.00000000 +00000-0 +98400-4 0 00004
2 62081 97.9020 305.1146 0004114 16.4107 343.7233 14.72292720 06
| Epoch (UTC): | 25 May 2026 15:09:52 |
| Eccentricity: | 0.0004114 |
| inclination: | 97.9020° |
| perigee height: | 651 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 305.1146° |
| argument of perigee: | 16.4107° |
| revolutions per day: | 14.72292720 |
| mean anomaly at epoch: | 343.7233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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