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 25191.56617340 .00000293 00000-0 31076-4 0 9992
2 16720 82.5530 13.5561 0020924 97.3067 322.9555 14.85365967 94920
| Epoch (UTC): | 10 July 2025 13:35:17 |
| Eccentricity: | 0.0020924 |
| inclination: | 82.5530° |
| perigee height: | 598 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 13.5561° |
| argument of perigee: | 97.3067° |
| revolutions per day: | 14.85365967 |
| mean anomaly at epoch: | 322.9555° |
| orbit number at epoch: | 9492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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