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 36302U 75087C 24357.71286073 .00000146 00000-0 72396-4 0 9998
2 36302 81.2485 240.7617 0109786 205.4862 218.1025 14.09573477814626
| Epoch (UTC): | 22 December 2024 17:06:31 |
| Eccentricity: | 0.0109786 |
| inclination: | 81.2485° |
| perigee height: | 781 km |
| apogee height: | 940 km |
| right ascension of ascending node: | 240.7617° |
| argument of perigee: | 205.4862° |
| revolutions per day: | 14.09573477 |
| mean anomaly at epoch: | 218.1025° |
| orbit number at epoch: | 81462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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