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 31734U 99025CEH 24355.25529661 .00002232 00000-0 86713-3 0 9995
2 31734 98.4774 351.0833 0105136 338.8776 20.8080 14.27849252913476
| Epoch (UTC): | 20 December 2024 06:07:37 |
| Eccentricity: | 0.0105136 |
| inclination: | 98.4774° |
| perigee height: | 723 km |
| apogee height: | 874 km |
| right ascension of ascending node: | 351.0833° |
| argument of perigee: | 338.8776° |
| revolutions per day: | 14.27849252 |
| mean anomaly at epoch: | 20.8080° |
| orbit number at epoch: | 91347 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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