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 16262U 85108A 22228.85203996 .00003566 00000-0 19822-3 0 9992
2 16262 82.4779 194.1286 0008882 263.5589 96.4631 15.13373351 3500
| Epoch (UTC): | 16 August 2022 20:26:56 |
| Eccentricity: | 0.0008882 |
| inclination: | 82.4779° |
| perigee height: | 520 km |
| apogee height: | 532 km |
| right ascension of ascending node: | 194.1286° |
| argument of perigee: | 263.5589° |
| revolutions per day: | 15.13373351 |
| mean anomaly at epoch: | 96.4631° |
| orbit number at epoch: | 350 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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