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 22889U 93070B 23337.56094500 .00000101 00000-0 84043-4 0 9990
2 22889 82.9460 1.3612 0051236 92.5282 268.1743 13.78069013512443
| Epoch (UTC): | 03 December 2023 13:27:45 |
| Eccentricity: | 0.0051236 |
| inclination: | 82.9460° |
| perigee height: | 933 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 1.3612° |
| argument of perigee: | 92.5282° |
| revolutions per day: | 13.78069013 |
| mean anomaly at epoch: | 268.1743° |
| orbit number at epoch: | 51244 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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