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 20805U 90083B 25198.53651895 .00000132 00000-0 11975-3 0 9994
2 20805 82.9352 28.5070 0031930 66.7381 346.3648 13.76200919749131
| Epoch (UTC): | 17 July 2025 12:52:35 |
| Eccentricity: | 0.0031930 |
| inclination: | 82.9352° |
| perigee height: | 954 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 28.5070° |
| argument of perigee: | 66.7381° |
| revolutions per day: | 13.76200919 |
| mean anomaly at epoch: | 346.3648° |
| orbit number at epoch: | 74913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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