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 12785U 81082A 24282.10114903 .00041828 00000-0 10998-2 0 9991
2 12785 82.4921 298.8783 0002078 123.5300 236.6144 15.38398959357480
| Epoch (UTC): | 08 October 2024 02:25:39 |
| Eccentricity: | 0.0002078 |
| inclination: | 82.4921° |
| perigee height: | 449 km |
| apogee height: | 452 km |
| right ascension of ascending node: | 298.8783° |
| argument of perigee: | 123.5300° |
| revolutions per day: | 15.38398959 |
| mean anomaly at epoch: | 236.6144° |
| orbit number at epoch: | 35748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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