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 29658U 06060A 22237.96953464 0.00004500 00000-0 16410-3 0 01
2 29658 98.1018 127.7326 0005209 0.9062 359.0937 15.28180769 03
| Epoch (UTC): | 25 August 2022 23:16:07 |
| Eccentricity: | 0.0005209 |
| inclination: | 98.1018° |
| perigee height: | 477 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 127.7326° |
| argument of perigee: | 0.9062° |
| revolutions per day: | 15.28180769 |
| mean anomaly at epoch: | 359.0937° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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