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 35080U 97051PF 24279.40464325 .00054588 00000-0 14653-1 0 9990
2 35080 86.2324 251.3268 0119856 214.0029 145.3452 14.43616309633562
| Epoch (UTC): | 05 October 2024 09:42:41 |
| Eccentricity: | 0.0119856 |
| inclination: | 86.2324° |
| perigee height: | 661 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 251.3268° |
| argument of perigee: | 214.0029° |
| revolutions per day: | 14.43616309 |
| mean anomaly at epoch: | 145.3452° |
| orbit number at epoch: | 63356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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