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 45117U 19071G 23030.31678783 .00586937 15474-3 14051-2 0 9992
2 45117 51.6219 352.7832 0004494 123.9225 236.2211 15.95951750168851
| Epoch (UTC): | 30 January 2023 07:36:10 |
| Eccentricity: | 0.0004494 |
| inclination: | 51.6219° |
| perigee height: | 282 km |
| apogee height: | 288 km |
| right ascension of ascending node: | 352.7832° |
| argument of perigee: | 123.9225° |
| revolutions per day: | 15.95951750 |
| mean anomaly at epoch: | 236.2211° |
| orbit number at epoch: | 16885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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