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 52108U 26145.27348750 +.00000000 +00000-0 +13930-4 0 00003
2 52108 53.2130 95.3209 0001404 70.8411 289.2733 15.08837057 08
| Epoch (UTC): | 25 May 2026 06:33:49 |
| Eccentricity: | 0.0001404 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.3209° |
| argument of perigee: | 70.8411° |
| revolutions per day: | 15.08837057 |
| mean anomaly at epoch: | 289.2733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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