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 52869U 26145.41378705 +.00000000 +00000-0 -14777-4 0 00007
2 52869 53.2138 29.6940 0001051 84.4544 275.6568 15.08840574 01
| Epoch (UTC): | 25 May 2026 09:55:51 |
| Eccentricity: | 0.0001051 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 29.6940° |
| argument of perigee: | 84.4544° |
| revolutions per day: | 15.08840574 |
| mean anomaly at epoch: | 275.6568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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