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 00082U 61004B 24254.67145266 .00002228 00000-0 18835-2 0 9996
2 00082 38.8542 232.5764 1165502 347.3506 10.0128 12.27000629997612
| Epoch (UTC): | 10 September 2024 16:06:53 |
| Eccentricity: | 0.1165502 |
| inclination: | 38.8542° |
| perigee height: | 637 km |
| apogee height: | 2487 km |
| right ascension of ascending node: | 232.5764° |
| argument of perigee: | 347.3506° |
| revolutions per day: | 12.27000629 |
| mean anomaly at epoch: | 10.0128° |
| orbit number at epoch: | 99761 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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