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 27431U 02024B 24261.13241281 .00000220 00000-0 15040-3 0 9999
2 27431 99.0469 300.2302 0014645 233.3038 126.6786 14.10030090149624
| Epoch (UTC): | 17 September 2024 03:10:40 |
| Eccentricity: | 0.0014645 |
| inclination: | 99.0469° |
| perigee height: | 848 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 300.2302° |
| argument of perigee: | 233.3038° |
| revolutions per day: | 14.10030090 |
| mean anomaly at epoch: | 126.6786° |
| orbit number at epoch: | 14962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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