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 23268.57007995 .00055168 00000-0 14286-2 0 9997
2 37854 101.6969 291.0408 0095978 70.8230 290.3355 15.34211842652307
| Epoch (UTC): | 25 September 2023 13:40:54 |
| Eccentricity: | 0.0095978 |
| inclination: | 101.6969° |
| perigee height: | 397 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 291.0408° |
| argument of perigee: | 70.8230° |
| revolutions per day: | 15.34211842 |
| mean anomaly at epoch: | 290.3355° |
| orbit number at epoch: | 65230 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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