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 30251U 99025XL 24357.77608394 .00002716 00000-0 10992-2 0 9990
2 30251 99.0560 176.5434 0052341 276.4387 213.3411 14.27922720930737
| Epoch (UTC): | 22 December 2024 18:37:33 |
| Eccentricity: | 0.0052341 |
| inclination: | 99.0560° |
| perigee height: | 761 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 176.5434° |
| argument of perigee: | 276.4387° |
| revolutions per day: | 14.27922720 |
| mean anomaly at epoch: | 213.3411° |
| orbit number at epoch: | 93073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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