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 22006U 92036A 23082.88283910 .00000113 00000-0 10262-3 0 9993
2 22006 82.9361 214.4059 0036249 331.5150 143.9569 13.75012897541772
| Epoch (UTC): | 23 March 2023 21:11:17 |
| Eccentricity: | 0.0036249 |
| inclination: | 82.9361° |
| perigee height: | 955 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 214.4059° |
| argument of perigee: | 331.5150° |
| revolutions per day: | 13.75012897 |
| mean anomaly at epoch: | 143.9569° |
| orbit number at epoch: | 54177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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