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 29196U 76103J 24275.24874022 .00000803 00000-0 75208-3 0 9999
2 29196 64.6981 201.1621 0063916 330.4642 105.8642 13.86919341568531
| Epoch (UTC): | 01 October 2024 05:58:11 |
| Eccentricity: | 0.0063916 |
| inclination: | 64.6981° |
| perigee height: | 892 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 201.1621° |
| argument of perigee: | 330.4642° |
| revolutions per day: | 13.86919341 |
| mean anomaly at epoch: | 105.8642° |
| orbit number at epoch: | 56853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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