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 54790U 26145.13822130 +.00000000 +00000-0 +14329-4 0 00009
2 54790 53.2129 45.7178 0001198 79.0430 281.0696 15.08837461 08
| Epoch (UTC): | 25 May 2026 03:19:02 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 45.7178° |
| argument of perigee: | 79.0430° |
| revolutions per day: | 15.08837461 |
| mean anomaly at epoch: | 281.0696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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