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 8294U 75087B 24277.20151397 .00000512 00000-0 27359-3 0 9997
2 8294 81.2095 304.6870 0107860 81.6108 279.7272 14.08917493520058
| Epoch (UTC): | 03 October 2024 04:50:10 |
| Eccentricity: | 0.0107860 |
| inclination: | 81.2095° |
| perigee height: | 785 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 304.6870° |
| argument of perigee: | 81.6108° |
| revolutions per day: | 14.08917493 |
| mean anomaly at epoch: | 279.7272° |
| orbit number at epoch: | 52005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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