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 51080U 22002DA 23155.42056552 .00019563 00000-0 71282-3 0 9992
2 51080 97.4616 226.1266 0008951 305.2335 54.8066 15.28192846 76949
| Epoch (UTC): | 04 June 2023 10:05:36 |
| Eccentricity: | 0.0008951 |
| inclination: | 97.4616° |
| perigee height: | 475 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 226.1266° |
| argument of perigee: | 305.2335° |
| revolutions per day: | 15.28192846 |
| mean anomaly at epoch: | 54.8066° |
| orbit number at epoch: | 7694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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