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 42844U 17042V 23268.52507436 .00008853 00000-0 75513-3 0 9997
2 42844 97.3815 105.2124 0009570 220.0418 140.0101 14.97904447337807
| Epoch (UTC): | 25 September 2023 12:36:06 |
| Eccentricity: | 0.0009570 |
| inclination: | 97.3815° |
| perigee height: | 567 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 105.2124° |
| argument of perigee: | 220.0418° |
| revolutions per day: | 14.97904447 |
| mean anomaly at epoch: | 140.0101° |
| orbit number at epoch: | 33780 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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