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 23271.11104116 -.00000144 00000-0 -49876-4 0 9990
2 31793 70.9743 250.3523 0003043 272.2069 157.9200 14.14556785839081
| Epoch (UTC): | 28 September 2023 02:39:53 |
| Eccentricity: | 0.0003043 |
| inclination: | 70.9743° |
| perigee height: | 841 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 250.3523° |
| argument of perigee: | 272.2069° |
| revolutions per day: | 14.14556785 |
| mean anomaly at epoch: | 157.9200° |
| orbit number at epoch: | 83908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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