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 51801U 26145.32593421 +.00000000 +00000-0 +37358-3 0 00004
2 51801 53.2134 5.0869 0001340 97.1845 262.9300 15.08817991 06
| Epoch (UTC): | 25 May 2026 07:49:20 |
| Eccentricity: | 0.0001340 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 5.0869° |
| argument of perigee: | 97.1845° |
| revolutions per day: | 15.08817991 |
| mean anomaly at epoch: | 262.9300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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