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 22176.91167366 .00000069 00000-0 50528-4 0 9993
2 24954 82.9226 352.5747 0040849 77.5792 33.1224 13.80055953246679
| Epoch (UTC): | 25 June 2022 21:52:48 |
| Eccentricity: | 0.0040849 |
| inclination: | 82.9226° |
| perigee height: | 933 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 352.5747° |
| argument of perigee: | 77.5792° |
| revolutions per day: | 13.80055953 |
| mean anomaly at epoch: | 33.1224° |
| orbit number at epoch: | 24667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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