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 42791U 17036AC 23337.63753797 .00295393 00000-0 14443-2 0 9994
2 42791 97.1129 16.8053 0003111 151.3707 208.7733 15.81515507359439
| Epoch (UTC): | 03 December 2023 15:18:03 |
| Eccentricity: | 0.0003111 |
| inclination: | 97.1129° |
| perigee height: | 324 km |
| apogee height: | 328 km |
| right ascension of ascending node: | 16.8053° |
| argument of perigee: | 151.3707° |
| revolutions per day: | 15.81515507 |
| mean anomaly at epoch: | 208.7733° |
| orbit number at epoch: | 35943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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