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 22803U 93059B 24254.84736796 .00000446 00000-0 24484-3 0 9997
2 22803 70.9890 79.9732 0018727 315.3334 44.6281 14.17066688602341
| Epoch (UTC): | 10 September 2024 20:20:12 |
| Eccentricity: | 0.0018727 |
| inclination: | 70.9890° |
| perigee height: | 822 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 79.9732° |
| argument of perigee: | 315.3334° |
| revolutions per day: | 14.17066688 |
| mean anomaly at epoch: | 44.6281° |
| orbit number at epoch: | 60234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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