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 25338U 98030A 24338.32403224 .00000494 00000-0 22151-3 0 9992
2 25338 98.5540 1.8244 0010159 184.3222 175.7872 14.26814776381556
| Epoch (UTC): | 03 December 2024 07:46:36 |
| Eccentricity: | 0.0010159 |
| inclination: | 98.5540° |
| perigee height: | 795 km |
| apogee height: | 809 km |
| right ascension of ascending node: | 1.8244° |
| argument of perigee: | 184.3222° |
| revolutions per day: | 14.26814776 |
| mean anomaly at epoch: | 175.7872° |
| orbit number at epoch: | 38155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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