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 39969U 87068CV 24355.76548936 .00011598 00000-0 39242-2 0 9998
2 39969 82.5014 3.7967 0014276 79.9265 280.3534 14.36692598546742
| Epoch (UTC): | 20 December 2024 18:22:18 |
| Eccentricity: | 0.0014276 |
| inclination: | 82.5014° |
| perigee height: | 759 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.7967° |
| argument of perigee: | 79.9265° |
| revolutions per day: | 14.36692598 |
| mean anomaly at epoch: | 280.3534° |
| orbit number at epoch: | 54674 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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