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 31792U 07029A 24287.51685793 .00000548 00000-0 32090-3 0 9991
2 31792 70.9360 198.4135 0009746 248.9691 111.0388 14.12754952891757
| Epoch (UTC): | 13 October 2024 12:24:16 |
| Eccentricity: | 0.0009746 |
| inclination: | 70.9360° |
| perigee height: | 843 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 198.4135° |
| argument of perigee: | 248.9691° |
| revolutions per day: | 14.12754952 |
| mean anomaly at epoch: | 111.0388° |
| orbit number at epoch: | 89175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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