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 05175U 71035B 23155.45893935 .00000237 00000-0 85934-4 0 9991
2 05175 74.0463 160.2705 0030059 191.7551 168.2906 14.38361323727788
| Epoch (UTC): | 04 June 2023 11:00:52 |
| Eccentricity: | 0.0030059 |
| inclination: | 74.0463° |
| perigee height: | 742 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 160.2705° |
| argument of perigee: | 191.7551° |
| revolutions per day: | 14.38361323 |
| mean anomaly at epoch: | 168.2906° |
| orbit number at epoch: | 72778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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