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 39976U 87068DC 24355.41704842 .00002102 00000-0 13660-2 0 9995
2 39976 82.5464 244.3242 0009195 99.7646 260.4563 14.02127516 55938
| Epoch (UTC): | 20 December 2024 10:00:32 |
| Eccentricity: | 0.0009195 |
| inclination: | 82.5464° |
| perigee height: | 880 km |
| apogee height: | 893 km |
| right ascension of ascending node: | 244.3242° |
| argument of perigee: | 99.7646° |
| revolutions per day: | 14.02127516 |
| mean anomaly at epoch: | 260.4563° |
| orbit number at epoch: | 5593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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