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 54810U 26145.40180292 +.00000000 +00000-0 +93002-4 0 00003
2 54810 53.2134 39.5159 0001695 88.4292 271.6894 15.08838565 00
| Epoch (UTC): | 25 May 2026 09:38:35 |
| Eccentricity: | 0.0001695 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.5159° |
| argument of perigee: | 88.4292° |
| revolutions per day: | 15.08838565 |
| mean anomaly at epoch: | 271.6894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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