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 23152.22742552 .00000179 00000-0 11826-3 0 9991
2 31793 70.9730 140.1342 0001641 265.6006 106.1025 14.14532520822276
| Epoch (UTC): | 01 June 2023 05:27:29 |
| Eccentricity: | 0.0001641 |
| inclination: | 70.9730° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 140.1342° |
| argument of perigee: | 265.6006° |
| revolutions per day: | 14.14532520 |
| mean anomaly at epoch: | 106.1025° |
| orbit number at epoch: | 82227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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