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 22286U 92094A 23157.39375195 .00002066 00000-0 21031-3 0 9998
2 22286 82.5189 116.1984 0022387 78.5041 281.8689 14.90082594625706
| Epoch (UTC): | 06 June 2023 09:27:00 |
| Eccentricity: | 0.0022387 |
| inclination: | 82.5189° |
| perigee height: | 582 km |
| apogee height: | 613 km |
| right ascension of ascending node: | 116.1984° |
| argument of perigee: | 78.5041° |
| revolutions per day: | 14.90082594 |
| mean anomaly at epoch: | 281.8689° |
| orbit number at epoch: | 62570 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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