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 52851U 26145.40919865 +.00000000 +00000-0 +41750-3 0 00004
2 52851 53.2131 39.7119 0001496 96.5481 263.5682 15.08808784 02
| Epoch (UTC): | 25 May 2026 09:49:14 |
| Eccentricity: | 0.0001496 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.7119° |
| argument of perigee: | 96.5481° |
| revolutions per day: | 15.08808784 |
| mean anomaly at epoch: | 263.5682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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