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 52102U 26145.30388634 +.00000000 +00000-0 +66736-4 0 00008
2 52102 53.2148 95.1860 0001338 78.8057 281.3085 15.08838392 08
| Epoch (UTC): | 25 May 2026 07:17:35 |
| Eccentricity: | 0.0001338 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.1860° |
| argument of perigee: | 78.8057° |
| revolutions per day: | 15.08838392 |
| mean anomaly at epoch: | 281.3085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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