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 22228.12508865 .00000765 00000-0 78775-4 0 9991
2 22286 82.5194 34.4259 0020260 341.3090 18.7382 14.88834956602977
| Epoch (UTC): | 16 August 2022 03:00:07 |
| Eccentricity: | 0.0020260 |
| inclination: | 82.5194° |
| perigee height: | 587 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 34.4259° |
| argument of perigee: | 341.3090° |
| revolutions per day: | 14.88834956 |
| mean anomaly at epoch: | 18.7382° |
| orbit number at epoch: | 60297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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