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 52107U 26145.26612751 +.00000000 +00000-0 +88576-4 0 00004
2 52107 53.2133 95.3546 0001493 87.7568 272.3595 15.08832715 07
| Epoch (UTC): | 25 May 2026 06:23:13 |
| Eccentricity: | 0.0001493 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 95.3546° |
| argument of perigee: | 87.7568° |
| revolutions per day: | 15.08832715 |
| mean anomaly at epoch: | 272.3595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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