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 24358.16032469 .00000116 00000-0 98697-4 0 9992
2 22889 82.9457 74.3176 0051117 91.2210 269.4804 13.78180681565804
| Epoch (UTC): | 23 December 2024 03:50:52 |
| Eccentricity: | 0.0051117 |
| inclination: | 82.9457° |
| perigee height: | 933 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 74.3176° |
| argument of perigee: | 91.2210° |
| revolutions per day: | 13.78180681 |
| mean anomaly at epoch: | 269.4804° |
| orbit number at epoch: | 56580 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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