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 31793U 07029B 23156.89647380 .00000275 00000-0 16832-3 0 9990
2 31793 70.9737 130.3240 0001599 269.2450 111.6824 14.14535254822844
| Epoch (UTC): | 05 June 2023 21:30:55 |
| Eccentricity: | 0.0001599 |
| inclination: | 70.9737° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 130.3240° |
| argument of perigee: | 269.2450° |
| revolutions per day: | 14.14535254 |
| mean anomaly at epoch: | 111.6824° |
| orbit number at epoch: | 82284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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