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 27433U 02024D 24279.09060022 .00002455 00000-0 13189-2 0 9990
2 27433 99.0029 314.8967 0015420 98.7826 261.5093 14.13808561153697
| Epoch (UTC): | 05 October 2024 02:10:27 |
| Eccentricity: | 0.0015420 |
| inclination: | 99.0029° |
| perigee height: | 835 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 314.8967° |
| argument of perigee: | 98.7826° |
| revolutions per day: | 14.13808561 |
| mean anomaly at epoch: | 261.5093° |
| orbit number at epoch: | 15369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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