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 12659U 81053P 24277.20034387 .00005116 00000-0 42154-2 0 9990
2 12659 82.7470 347.2110 0068697 179.4829 248.6309 13.87854459168503
| Epoch (UTC): | 03 October 2024 04:48:29 |
| Eccentricity: | 0.0068697 |
| inclination: | 82.7470° |
| perigee height: | 886 km |
| apogee height: | 986 km |
| right ascension of ascending node: | 347.2110° |
| argument of perigee: | 179.4829° |
| revolutions per day: | 13.87854459 |
| mean anomaly at epoch: | 248.6309° |
| orbit number at epoch: | 16850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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