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 40783U 89006CC 24242.65588814 -.00000098 00000-0 97751-2 0 9993
2 40783 6.6817 250.9329 7040634 122.7025 348.3225 2.24621294153878
| Epoch (UTC): | 29 August 2024 15:44:28 |
| Eccentricity: | 0.7040634 |
| inclination: | 6.6817° |
| perigee height: | 910 km |
| apogee height: | 35590 km |
| right ascension of ascending node: | 250.9329° |
| argument of perigee: | 122.7025° |
| revolutions per day: | 2.24621294 |
| mean anomaly at epoch: | 348.3225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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