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 39669U 87060AG 24356.87587282 .00000895 00000-0 35971-3 0 9991
2 39669 65.0135 94.5602 0019658 259.2463 100.6409 14.33337111559883
| Epoch (UTC): | 21 December 2024 21:01:15 |
| Eccentricity: | 0.0019658 |
| inclination: | 65.0135° |
| perigee height: | 766 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 94.5602° |
| argument of perigee: | 259.2463° |
| revolutions per day: | 14.33337111 |
| mean anomaly at epoch: | 100.6409° |
| orbit number at epoch: | 55988 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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