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 22287U 92094B 24257.71214835 .00001550 00000-0 20471-3 0 9994
2 22287 82.5247 137.3871 0023112 316.1001 43.8374 14.79268849709409
| Epoch (UTC): | 13 September 2024 17:05:29 |
| Eccentricity: | 0.0023112 |
| inclination: | 82.5247° |
| perigee height: | 615 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 137.3871° |
| argument of perigee: | 316.1001° |
| revolutions per day: | 14.79268849 |
| mean anomaly at epoch: | 43.8374° |
| orbit number at epoch: | 70940 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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