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 37854U 11061E 23342.54033908 .00041956 00000-0 87558-3 0 9993
2 37854 101.6828 48.4109 0081719 200.7687 159.0217 15.41850977663677
| Epoch (UTC): | 08 December 2023 12:58:05 |
| Eccentricity: | 0.0081719 |
| inclination: | 101.6828° |
| perigee height: | 385 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 48.4109° |
| argument of perigee: | 200.7687° |
| revolutions per day: | 15.41850977 |
| mean anomaly at epoch: | 159.0217° |
| orbit number at epoch: | 66367 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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