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 29051U 06011E 24280.85470950 .00002895 00000-0 11011-2 0 9999
2 29051 72.0029 126.7592 0065247 83.6054 277.2508 14.30462589966803
| Epoch (UTC): | 06 October 2024 20:30:46 |
| Eccentricity: | 0.0065247 |
| inclination: | 72.0029° |
| perigee height: | 743 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 126.7592° |
| argument of perigee: | 83.6054° |
| revolutions per day: | 14.30462589 |
| mean anomaly at epoch: | 277.2508° |
| orbit number at epoch: | 96680 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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