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 29050U 06011D 23338.51276089 .00002694 00000-0 54478-3 0 9993
2 29050 72.0143 150.0517 0047808 184.9106 175.1586 14.61434460941011
| Epoch (UTC): | 04 December 2023 12:18:22 |
| Eccentricity: | 0.0047808 |
| inclination: | 72.0143° |
| perigee height: | 655 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 150.0517° |
| argument of perigee: | 184.9106° |
| revolutions per day: | 14.61434460 |
| mean anomaly at epoch: | 175.1586° |
| orbit number at epoch: | 94101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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