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 24357.93777264 .00000644 00000-0 18263-3 0 9995
2 00045 66.6943 351.1003 0252821 195.8727 163.4348 14.35241688302351
| Epoch (UTC): | 22 December 2024 22:30:23 |
| Eccentricity: | 0.0252821 |
| inclination: | 66.6943° |
| perigee height: | 593 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 351.1003° |
| argument of perigee: | 195.8727° |
| revolutions per day: | 14.35241688 |
| mean anomaly at epoch: | 163.4348° |
| orbit number at epoch: | 30235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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