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 22175.43685532 .00000129 00000-0 59398-4 0 9995
2 00045 66.6937 238.5635 0250098 140.5349 221.4269 14.33866352171488
| Epoch (UTC): | 24 June 2022 10:29:04 |
| Eccentricity: | 0.0250098 |
| inclination: | 66.6937° |
| perigee height: | 600 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 238.5635° |
| argument of perigee: | 140.5349° |
| revolutions per day: | 14.33866352 |
| mean anomaly at epoch: | 221.4269° |
| orbit number at epoch: | 17148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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