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 42829U 17042E 24261.01580257 .00008389 00000-0 71628-3 0 9997
2 42829 97.3869 77.0291 0012704 122.9748 237.2698 14.97849554390917
| Epoch (UTC): | 17 September 2024 00:22:45 |
| Eccentricity: | 0.0012704 |
| inclination: | 97.3869° |
| perigee height: | 565 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 77.0291° |
| argument of perigee: | 122.9748° |
| revolutions per day: | 14.97849554 |
| mean anomaly at epoch: | 237.2698° |
| orbit number at epoch: | 39091 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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