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 52855U 26145.65943106 +.00000000 +00000-0 -10784-4 0 00005
2 52855 53.2133 38.5879 0001478 93.7910 266.3252 15.08835063 08
| Epoch (UTC): | 25 May 2026 15:49:34 |
| Eccentricity: | 0.0001478 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 38.5879° |
| argument of perigee: | 93.7910° |
| revolutions per day: | 15.08835063 |
| mean anomaly at epoch: | 266.3252° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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