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 22279.85319907 .00000276 00000-0 96776-4 0 9990
2 00045 66.6951 323.3404 0248116 62.3639 300.2411 14.33913216186452
| Epoch (UTC): | 06 October 2022 20:28:36 |
| Eccentricity: | 0.0248116 |
| inclination: | 66.6951° |
| perigee height: | 601 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 323.3404° |
| argument of perigee: | 62.3639° |
| revolutions per day: | 14.33913216 |
| mean anomaly at epoch: | 300.2411° |
| orbit number at epoch: | 18645 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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