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 23082.82757678 .00009710 00000-0 87134-3 0 9994
2 42844 97.3949 289.7491 0012160 128.0551 232.1770 14.95874165310025
| Epoch (UTC): | 23 March 2023 19:51:42 |
| Eccentricity: | 0.0012160 |
| inclination: | 97.3949° |
| perigee height: | 571 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 289.7491° |
| argument of perigee: | 128.0551° |
| revolutions per day: | 14.95874165 |
| mean anomaly at epoch: | 232.1770° |
| orbit number at epoch: | 31002 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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