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 14781U 84021B 24340.84012418 .00003708 00000-0 40780-3 0 9997
2 14781 97.7300 305.3379 0006556 222.1532 137.9181 14.88190525195006
| Epoch (UTC): | 05 December 2024 20:09:46 |
| Eccentricity: | 0.0006556 |
| inclination: | 97.7300° |
| perigee height: | 599 km |
| apogee height: | 608 km |
| right ascension of ascending node: | 305.3379° |
| argument of perigee: | 222.1532° |
| revolutions per day: | 14.88190525 |
| mean anomaly at epoch: | 137.9181° |
| orbit number at epoch: | 19500 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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