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 33493U 09002B 23339.91079502 .00012918 00000-0 77072-3 0 9993
2 33493 98.2332 6.9457 0014185 183.6558 176.4568 15.11211613809632
| Epoch (UTC): | 05 December 2023 21:51:32 |
| Eccentricity: | 0.0014185 |
| inclination: | 98.2332° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 6.9457° |
| argument of perigee: | 183.6558° |
| revolutions per day: | 15.11211613 |
| mean anomaly at epoch: | 176.4568° |
| orbit number at epoch: | 80963 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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