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 52835U 26145.46346836 +.00000000 +00000-0 +14936-4 0 00001
2 52835 53.2139 49.4692 0002287 108.6012 251.5228 15.08839132 04
| Epoch (UTC): | 25 May 2026 11:07:23 |
| Eccentricity: | 0.0002287 |
| inclination: | 53.2139° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.4692° |
| argument of perigee: | 108.6012° |
| revolutions per day: | 15.08839132 |
| mean anomaly at epoch: | 251.5228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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