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 34765U 97051LJ 24358.00097806 .00002942 00000-0 94688-3 0 9994
2 34765 86.3418 184.7550 0015464 310.5205 177.7289 14.38968712825884
| Epoch (UTC): | 23 December 2024 00:01:24 |
| Eccentricity: | 0.0015464 |
| inclination: | 86.3418° |
| perigee height: | 751 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 184.7550° |
| argument of perigee: | 310.5205° |
| revolutions per day: | 14.38968712 |
| mean anomaly at epoch: | 177.7289° |
| orbit number at epoch: | 82588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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