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 53789U 26145.41927381 +.00000000 +00000-0 +38916-3 0 00008
2 53789 53.2146 289.3889 0001599 76.2881 283.8289 15.08849354 05
| Epoch (UTC): | 25 May 2026 10:03:45 |
| Eccentricity: | 0.0001599 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.3889° |
| argument of perigee: | 76.2881° |
| revolutions per day: | 15.08849354 |
| mean anomaly at epoch: | 283.8289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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