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 30041U 99025NS 22222.86632007 .00000365 00000-0 23222-3 0 9993
2 30041 99.5619 242.5392 0036177 2.0163 121.8212 14.10418359800766
| Epoch (UTC): | 10 August 2022 20:47:30 |
| Eccentricity: | 0.0036177 |
| inclination: | 99.5619° |
| perigee height: | 832 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 242.5392° |
| argument of perigee: | 2.0163° |
| revolutions per day: | 14.10418359 |
| mean anomaly at epoch: | 121.8212° |
| orbit number at epoch: | 80076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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