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 51793U 26145.66668980 +.00000000 +00000-0 +14163-2 0 00002
2 51793 53.2156 329.7407 0000489 77.6952 96.6642 15.91736110 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000489 |
| inclination: | 53.2156° |
| perigee height: | 297 km |
| apogee height: | 298 km |
| right ascension of ascending node: | 329.7407° |
| argument of perigee: | 77.6952° |
| revolutions per day: | 15.91736110 |
| mean anomaly at epoch: | 96.6642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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