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 11672U 80005B 25188.05580131 .00000408 00000-0 39146-4 0 9996
2 11672 82.5141 180.1384 0014231 261.5211 98.4395 14.90526312439898
| Epoch (UTC): | 07 July 2025 01:20:21 |
| Eccentricity: | 0.0014231 |
| inclination: | 82.5141° |
| perigee height: | 586 km |
| apogee height: | 606 km |
| right ascension of ascending node: | 180.1384° |
| argument of perigee: | 261.5211° |
| revolutions per day: | 14.90526312 |
| mean anomaly at epoch: | 98.4395° |
| orbit number at epoch: | 43989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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