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 16612U 86018B 24281.80833672 .00001997 00000-0 22683-3 0 9993
2 16612 82.5144 310.5061 0016539 342.6740 17.3909 14.85753974966416
| Epoch (UTC): | 07 October 2024 19:24:00 |
| Eccentricity: | 0.0016539 |
| inclination: | 82.5144° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 310.5061° |
| argument of perigee: | 342.6740° |
| revolutions per day: | 14.85753974 |
| mean anomaly at epoch: | 17.3909° |
| orbit number at epoch: | 96641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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