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 14680U 84010B 25188.95376628 .00000001 00000-0 -14761-4 0 9997
2 14680 82.9560 19.8135 0039124 101.7542 7.7992 13.76697182 80661
| Epoch (UTC): | 07 July 2025 22:53:25 |
| Eccentricity: | 0.0039124 |
| inclination: | 82.9560° |
| perigee height: | 947 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 19.8135° |
| argument of perigee: | 101.7542° |
| revolutions per day: | 13.76697182 |
| mean anomaly at epoch: | 7.7992° |
| orbit number at epoch: | 8066 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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