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 69031U 26145.52741815 +.00000000 +00000-0 -13544-2 0 00003
2 69031 97.2846 0.3003 0001377 93.2581 266.8842 15.74971089 06
| Epoch (UTC): | 25 May 2026 12:39:28 |
| Eccentricity: | 0.0001377 |
| inclination: | 97.2846° |
| perigee height: | 344 km |
| apogee height: | 346 km |
| right ascension of ascending node: | 0.3003° |
| argument of perigee: | 93.2581° |
| revolutions per day: | 15.74971089 |
| mean anomaly at epoch: | 266.8842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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