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 40024U 14033Q 22024.82074247 .00000977 00000-0 10495-3 0 9990
2 40024 97.9725 326.7740 0012487 154.1986 205.9857 14.90859172413095
| Epoch (UTC): | 24 January 2022 19:41:52 |
| Eccentricity: | 0.0012487 |
| inclination: | 97.9725° |
| perigee height: | 586 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 326.7740° |
| argument of perigee: | 154.1986° |
| revolutions per day: | 14.90859172 |
| mean anomaly at epoch: | 205.9857° |
| orbit number at epoch: | 41309 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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