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 25544U 98067A 22221.92646991 .00006058 00000-0 11289-3 0 9998
2 25544 51.6448 70.3700 0005152 101.7041 98.6467 15.50292585353513
| Epoch (UTC): | 09 August 2022 22:14:07 |
| Eccentricity: | 0.0005152 |
| inclination: | 51.6448° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 70.3700° |
| argument of perigee: | 101.7041° |
| revolutions per day: | 15.50292585 |
| mean anomaly at epoch: | 98.6467° |
| orbit number at epoch: | 35351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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