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 52895U 26145.40126441 +.00000000 +00000-0 +16008-4 0 00001
2 52895 98.2313 285.4715 0009527 105.3377 254.8876 14.58687599 00
| Epoch (UTC): | 25 May 2026 09:37:49 |
| Eccentricity: | 0.0009527 |
| inclination: | 98.2313° |
| perigee height: | 691 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 285.4715° |
| argument of perigee: | 105.3377° |
| revolutions per day: | 14.58687599 |
| mean anomaly at epoch: | 254.8876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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