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 65107U 26145.59904433 +.00000000 +00000-0 +11112-3 0 00006
2 65107 50.0012 46.8297 0009320 21.9216 338.2054 13.29317506 02
| Epoch (UTC): | 25 May 2026 14:22:37 |
| Eccentricity: | 0.0009320 |
| inclination: | 50.0012° |
| perigee height: | 1142 km |
| apogee height: | 1156 km |
| right ascension of ascending node: | 46.8297° |
| argument of perigee: | 21.9216° |
| revolutions per day: | 13.29317506 |
| mean anomaly at epoch: | 338.2054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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