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 25397U 98043D 24340.52674351 .00000333 00000-0 16438-3 0 9990
2 25397 98.9472 310.0270 0002032 52.3634 307.7728 14.24205403371808
| Epoch (UTC): | 05 December 2024 12:38:30 |
| Eccentricity: | 0.0002032 |
| inclination: | 98.9472° |
| perigee height: | 810 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 310.0270° |
| argument of perigee: | 52.3634° |
| revolutions per day: | 14.24205403 |
| mean anomaly at epoch: | 307.7728° |
| orbit number at epoch: | 37180 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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