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 04564U 70079A 23341.09921732 -.00000061 00000-0 24169-4 0 9992
2 04564 65.2778 242.9076 0049819 59.9244 300.6742 13.78487770675877
| Epoch (UTC): | 07 December 2023 02:22:52 |
| Eccentricity: | 0.0049819 |
| inclination: | 65.2778° |
| perigee height: | 932 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 242.9076° |
| argument of perigee: | 59.9244° |
| revolutions per day: | 13.78487770 |
| mean anomaly at epoch: | 300.6742° |
| orbit number at epoch: | 67587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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