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 23342.19723061 .00000206 00000-0 78454-4 0 9995
2 00045 66.6945 276.2436 0246273 112.4972 250.2402 14.34461649247737
| Epoch (UTC): | 08 December 2023 04:44:00 |
| Eccentricity: | 0.0246273 |
| inclination: | 66.6945° |
| perigee height: | 600 km |
| apogee height: | 953 km |
| right ascension of ascending node: | 276.2436° |
| argument of perigee: | 112.4972° |
| revolutions per day: | 14.34461649 |
| mean anomaly at epoch: | 250.2402° |
| orbit number at epoch: | 24773 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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