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 55107U 26145.63807854 +.00000000 +00000-0 +44772-3 0 00007
2 55107 97.9198 222.2952 0008991 4.0073 356.1215 14.91880496 01
| Epoch (UTC): | 25 May 2026 15:18:49 |
| Eccentricity: | 0.0008991 |
| inclination: | 97.9198° |
| perigee height: | 586 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 222.2952° |
| argument of perigee: | 4.0073° |
| revolutions per day: | 14.91880496 |
| mean anomaly at epoch: | 356.1215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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