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 16720U 86034B 24357.60650417 .00000806 00000-0 91330-4 0 9991
2 16720 82.5529 200.5546 0020581 42.5207 11.4613 14.85021291 65243
| Epoch (UTC): | 22 December 2024 14:33:21 |
| Eccentricity: | 0.0020581 |
| inclination: | 82.5529° |
| perigee height: | 599 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 200.5546° |
| argument of perigee: | 42.5207° |
| revolutions per day: | 14.85021291 |
| mean anomaly at epoch: | 11.4613° |
| orbit number at epoch: | 6524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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