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 22081U 92053B 24287.30417948 .00001250 00000-0 45054-3 0 9990
2 22081 74.0436 227.9203 0036840 261.9367 97.7604 14.34333838681715
| Epoch (UTC): | 13 October 2024 07:18:01 |
| Eccentricity: | 0.0036840 |
| inclination: | 74.0436° |
| perigee height: | 751 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 227.9203° |
| argument of perigee: | 261.9367° |
| revolutions per day: | 14.34333838 |
| mean anomaly at epoch: | 97.7604° |
| orbit number at epoch: | 68171 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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