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 18821U 88005B 23156.43161098 .00000021 00000-0 56199-5 0 9998
2 18821 82.5410 127.4578 0013724 333.3060 26.7393 13.85149153786675
| Epoch (UTC): | 05 June 2023 10:21:31 |
| Eccentricity: | 0.0013724 |
| inclination: | 82.5410° |
| perigee height: | 935 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 127.4578° |
| argument of perigee: | 333.3060° |
| revolutions per day: | 13.85149153 |
| mean anomaly at epoch: | 26.7393° |
| orbit number at epoch: | 78667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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