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 51997U 26144.98092490 +.00000000 +00000-0 -56189-4 0 00006
2 51997 53.2131 36.6339 0001815 91.4942 268.6258 15.08845079 06
| Epoch (UTC): | 24 May 2026 23:32:31 |
| Eccentricity: | 0.0001815 |
| inclination: | 53.2131° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 36.6339° |
| argument of perigee: | 91.4942° |
| revolutions per day: | 15.08845079 |
| mean anomaly at epoch: | 268.6258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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