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 42999U 74011C 24355.25711027 .00013877 00000-0 50124-2 0 9990
2 42999 81.2329 182.2883 0030337 101.0194 259.4404 14.33220564436522
| Epoch (UTC): | 20 December 2024 06:10:14 |
| Eccentricity: | 0.0030337 |
| inclination: | 81.2329° |
| perigee height: | 759 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 182.2883° |
| argument of perigee: | 101.0194° |
| revolutions per day: | 14.33220564 |
| mean anomaly at epoch: | 259.4404° |
| orbit number at epoch: | 43652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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