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 24773U 97017B 25189.56108398 .00000099 00000-0 89648-4 0 9999
2 24773 82.9220 351.5208 0025109 37.3149 30.1462 13.73928324414722
| Epoch (UTC): | 08 July 2025 13:27:57 |
| Eccentricity: | 0.0025109 |
| inclination: | 82.9220° |
| perigee height: | 967 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 351.5208° |
| argument of perigee: | 37.3149° |
| revolutions per day: | 13.73928324 |
| mean anomaly at epoch: | 30.1462° |
| orbit number at epoch: | 41472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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