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 22237U 92080B 24340.43355901 .00001248 00000-0 16277-3 0 9999
2 22237 82.5111 98.6910 0017881 281.1384 78.7819 14.79734260726504
| Epoch (UTC): | 05 December 2024 10:24:19 |
| Eccentricity: | 0.0017881 |
| inclination: | 82.5111° |
| perigee height: | 617 km |
| apogee height: | 642 km |
| right ascension of ascending node: | 98.6910° |
| argument of perigee: | 281.1384° |
| revolutions per day: | 14.79734260 |
| mean anomaly at epoch: | 78.7819° |
| orbit number at epoch: | 72650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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