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 53950U 22121C 24279.85794752 .00058125 00000-0 13930-2 0 9990
2 53950 97.3788 305.2403 0008669 169.4261 190.7169 15.41178792112834
| Epoch (UTC): | 05 October 2024 20:35:26 |
| Eccentricity: | 0.0008669 |
| inclination: | 97.3788° |
| perigee height: | 437 km |
| apogee height: | 448 km |
| right ascension of ascending node: | 305.2403° |
| argument of perigee: | 169.4261° |
| revolutions per day: | 15.41178792 |
| mean anomaly at epoch: | 190.7169° |
| orbit number at epoch: | 11283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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