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 19120U 88039B 23154.15871397 .00000210 00000-0 12281-3 0 9997
2 19120 71.0159 44.8060 0019741 90.0963 270.2424 14.19317440814984
| Epoch (UTC): | 03 June 2023 03:48:32 |
| Eccentricity: | 0.0019741 |
| inclination: | 71.0159° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 44.8060° |
| argument of perigee: | 90.0963° |
| revolutions per day: | 14.19317440 |
| mean anomaly at epoch: | 270.2424° |
| orbit number at epoch: | 81498 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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