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 36519U 10017A 25347.85859116 .00000060 00000-0 50278-4 0 9999
2 36519 82.9612 25.8905 0034783 284.8494 249.3134 13.71649225782527
| Epoch (UTC): | 13 December 2025 20:36:22 |
| Eccentricity: | 0.0034783 |
| inclination: | 82.9612° |
| perigee height: | 968 km |
| apogee height: | 1019 km |
| right ascension of ascending node: | 25.8905° |
| argument of perigee: | 284.8494° |
| revolutions per day: | 13.71649225 |
| mean anomaly at epoch: | 249.3134° |
| orbit number at epoch: | 78252 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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