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 22487U 93008A 23337.87921706 .00000122 00000-0 10993-3 0 9991
2 22487 82.9429 149.7132 0038045 182.2961 290.4114 13.75895364542930
| Epoch (UTC): | 03 December 2023 21:06:04 |
| Eccentricity: | 0.0038045 |
| inclination: | 82.9429° |
| perigee height: | 950 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 149.7132° |
| argument of perigee: | 182.2961° |
| revolutions per day: | 13.75895364 |
| mean anomaly at epoch: | 290.4114° |
| orbit number at epoch: | 54293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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