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 38829U 99025EVV 24357.01972789 .00001712 00000-0 10206-2 0 9991
2 38829 98.7725 17.0102 0041019 314.7258 45.0574 14.08180875591244
| Epoch (UTC): | 22 December 2024 00:28:24 |
| Eccentricity: | 0.0041019 |
| inclination: | 98.7725° |
| perigee height: | 836 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 17.0102° |
| argument of perigee: | 314.7258° |
| revolutions per day: | 14.08180875 |
| mean anomaly at epoch: | 45.0574° |
| orbit number at epoch: | 59124 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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