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 51031U 22002AZ 24034.97965628 .13195474 25060-5 11517-2 0 9990
2 51031 97.3842 117.3732 0010755 286.4771 73.5346 16.39193808114835
| Epoch (UTC): | 03 February 2024 23:30:42 |
| Eccentricity: | 0.0010755 |
| inclination: | 97.3842° |
| perigee height: | 161 km |
| apogee height: | 175 km |
| right ascension of ascending node: | 117.3732° |
| argument of perigee: | 286.4771° |
| revolutions per day: | 16.39193808 |
| mean anomaly at epoch: | 73.5346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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