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 24954U 97052B 23338.03201786 .00000159 00000-0 13747-3 0 9993
2 24954 82.9211 318.3504 0040456 38.9721 22.7779 13.80149714319221
| Epoch (UTC): | 04 December 2023 00:46:06 |
| Eccentricity: | 0.0040456 |
| inclination: | 82.9211° |
| perigee height: | 933 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 318.3504° |
| argument of perigee: | 38.9721° |
| revolutions per day: | 13.80149714 |
| mean anomaly at epoch: | 22.7779° |
| orbit number at epoch: | 31922 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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