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 04231U 69082CN 22221.42586574 .00000730 00000-0 23505-3 0 9993
2 04231 70.2788 113.4345 0036202 339.2506 20.7154 14.42578090748093
| Epoch (UTC): | 09 August 2022 10:13:14 |
| Eccentricity: | 0.0036202 |
| inclination: | 70.2788° |
| perigee height: | 724 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 113.4345° |
| argument of perigee: | 339.2506° |
| revolutions per day: | 14.42578090 |
| mean anomaly at epoch: | 20.7154° |
| orbit number at epoch: | 74809 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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