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 01002U 65008C 22225.90239385 .00000000 00000-0 -11208-2 0 9999
2 01002 32.1423 129.0151 0015613 238.7056 121.1912 9.88353813 77353
| Epoch (UTC): | 13 August 2022 21:39:26 |
| Eccentricity: | 0.0015613 |
| inclination: | 32.1423° |
| perigee height: | 2779 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 129.0151° |
| argument of perigee: | 238.7056° |
| revolutions per day: | 9.88353813 |
| mean anomaly at epoch: | 121.1912° |
| orbit number at epoch: | 7735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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