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 42544U 70025TA 22226.37017534 .00002798 00000-0 72936-3 0 9993
2 42544 98.6354 292.0245 0071614 344.6445 15.2574 14.48844565409342
| Epoch (UTC): | 14 August 2022 08:53:03 |
| Eccentricity: | 0.0071614 |
| inclination: | 98.6354° |
| perigee height: | 678 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 292.0245° |
| argument of perigee: | 344.6445° |
| revolutions per day: | 14.48844565 |
| mean anomaly at epoch: | 15.2574° |
| orbit number at epoch: | 40934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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