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 25131.90274322 .00000076 00000-0 58274-4 0 9991
2 24954 82.9201 284.9686 0039340 2.8510 161.5282 13.80306561391647
| Epoch (UTC): | 11 May 2025 21:39:57 |
| Eccentricity: | 0.0039340 |
| inclination: | 82.9201° |
| perigee height: | 934 km |
| apogee height: | 991 km |
| right ascension of ascending node: | 284.9686° |
| argument of perigee: | 2.8510° |
| revolutions per day: | 13.80306561 |
| mean anomaly at epoch: | 161.5282° |
| orbit number at epoch: | 39164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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