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 00045U 60007A 23342.82473367 .00000193 00000-0 75354-4 0 9997
2 00045 66.6945 274.5881 0246246 112.0270 250.7186 14.34462107247823
| Epoch (UTC): | 08 December 2023 19:47:36 |
| Eccentricity: | 0.0246246 |
| inclination: | 66.6945° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 274.5881° |
| argument of perigee: | 112.0270° |
| revolutions per day: | 14.34462107 |
| mean anomaly at epoch: | 250.7186° |
| orbit number at epoch: | 24782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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