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 51882U 26145.02788368 +.00000000 +00000-0 -17159-4 0 00005
2 51882 53.2133 16.4345 0001398 105.1124 255.0023 15.08846774 08
| Epoch (UTC): | 25 May 2026 00:40:09 |
| Eccentricity: | 0.0001398 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.4345° |
| argument of perigee: | 105.1124° |
| revolutions per day: | 15.08846774 |
| mean anomaly at epoch: | 255.0023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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