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 23862U 96029D 24115.94632903 0.00005400 00000-0 12336-2 0 05
2 23862 63.3293 75.3255 0805311 38.6923 321.3077 13.42712074 09
| Epoch (UTC): | 24 April 2024 22:42:42 |
| Eccentricity: | 0.0805311 |
| inclination: | 63.3293° |
| perigee height: | 497 km |
| apogee height: | 1701 km |
| right ascension of ascending node: | 75.3255° |
| argument of perigee: | 38.6923° |
| revolutions per day: | 13.42712074 |
| mean anomaly at epoch: | 321.3077° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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