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 65987U 26145.49250971 +.00000000 +00000-0 +82332-4 0 00005
2 65987 81.3004 233.2757 0001119 142.8734 217.2497 13.78596037 04
| Epoch (UTC): | 25 May 2026 11:49:12 |
| Eccentricity: | 0.0001119 |
| inclination: | 81.3004° |
| perigee height: | 968 km |
| apogee height: | 970 km |
| right ascension of ascending node: | 233.2757° |
| argument of perigee: | 142.8734° |
| revolutions per day: | 13.78596037 |
| mean anomaly at epoch: | 217.2497° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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