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 52850U 26145.45710836 +.00000000 +00000-0 +21777-4 0 00003
2 52850 53.2130 49.8553 0001263 101.6766 258.4368 15.08839536 03
| Epoch (UTC): | 25 May 2026 10:58:14 |
| Eccentricity: | 0.0001263 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.8553° |
| argument of perigee: | 101.6766° |
| revolutions per day: | 15.08839536 |
| mean anomaly at epoch: | 258.4368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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