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 23344.91640987 .00000147 00000-0 63696-4 0 9998
2 00045 66.6944 269.0697 0246179 110.4522 252.3195 14.34463098248125
| Epoch (UTC): | 10 December 2023 21:59:37 |
| Eccentricity: | 0.0246179 |
| inclination: | 66.6944° |
| perigee height: | 601 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 269.0697° |
| argument of perigee: | 110.4522° |
| revolutions per day: | 14.34463098 |
| mean anomaly at epoch: | 252.3195° |
| orbit number at epoch: | 24812 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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