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 14551U 83122A 23277.62384667 .00020690 00000-0 74091-3 0 9996
2 14551 82.4969 50.1560 0005033 193.0039 167.1072 15.28627477918864
| Epoch (UTC): | 04 October 2023 14:58:20 |
| Eccentricity: | 0.0005033 |
| inclination: | 82.4969° |
| perigee height: | 476 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 50.1560° |
| argument of perigee: | 193.0039° |
| revolutions per day: | 15.28627477 |
| mean anomaly at epoch: | 167.1072° |
| orbit number at epoch: | 91886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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