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 23027.35375599 .00000983 00000-0 26860-3 0 9997
2 00045 66.6946 26.7455 0257211 339.6470 19.4519 14.34025683202589
| Epoch (UTC): | 27 January 2023 08:29:24 |
| Eccentricity: | 0.0257211 |
| inclination: | 66.6946° |
| perigee height: | 594 km |
| apogee height: | 962 km |
| right ascension of ascending node: | 26.7455° |
| argument of perigee: | 339.6470° |
| revolutions per day: | 14.34025683 |
| mean anomaly at epoch: | 19.4519° |
| orbit number at epoch: | 20258 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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