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 is defined by the following mean orbital elements,
1 23936U 96029E 24115.96409339 0.00004900 00000-0 10807-2 0 09
2 23936 63.3278 73.9423 0811378 38.0362 321.9638 13.42724226 07
| Epoch (UTC): | 24 April 2024 23:08:17 |
| Eccentricity: | 0.0811378 |
| inclination: | 63.3278° |
| perigee height: | 492 km |
| apogee height: | 1706 km |
| right ascension of ascending node: | 73.9423° |
| argument of perigee: | 38.0362° |
| revolutions per day: | 13.42724226 |
| mean anomaly at epoch: | 321.9638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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