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 29982U 99025LG 24357.91542317 .00010142 00000-0 17839-2 0 9996
2 29982 99.3704 123.1359 0130860 285.3708 203.1948 14.62368021950924
| Epoch (UTC): | 22 December 2024 21:58:12 |
| Eccentricity: | 0.0130860 |
| inclination: | 99.3704° |
| perigee height: | 593 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 123.1359° |
| argument of perigee: | 285.3708° |
| revolutions per day: | 14.62368021 |
| mean anomaly at epoch: | 203.1948° |
| orbit number at epoch: | 95092 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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