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 data is extracted from the following two-line orbital elements,
1 36508U 10013A 25192.61708946 .00000183 00000-0 44755-4 0 9998
2 36508 92.0089 194.9835 0002513 82.1569 277.9923 14.51911249808667
| Epoch (UTC): | 11 July 2025 14:48:36 |
| Eccentricity: | 0.0002513 |
| inclination: | 92.0089° |
| perigee height: | 717 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 194.9835° |
| argument of perigee: | 82.1569° |
| revolutions per day: | 14.51911249 |
| mean anomaly at epoch: | 277.9923° |
| orbit number at epoch: | 80866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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