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 54024U 22127B 23335.03537636 .00004360 00000-0 55052-3 0 9991
2 54024 98.2875 349.3173 0134389 126.4547 234.9137 14.76224945 61777
| Epoch (UTC): | 01 December 2023 00:50:56 |
| Eccentricity: | 0.0134389 |
| inclination: | 98.2875° |
| perigee height: | 547 km |
| apogee height: | 735 km |
| right ascension of ascending node: | 349.3173° |
| argument of perigee: | 126.4547° |
| revolutions per day: | 14.76224945 |
| mean anomaly at epoch: | 234.9137° |
| orbit number at epoch: | 6177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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