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 20625U 90046B 25198.07774350 -.00000280 00000-0 -11961-3 0 9995
2 20625 70.9991 72.7233 0016260 298.3181 61.6301 14.14969028815064
| Epoch (UTC): | 17 July 2025 01:51:57 |
| Eccentricity: | 0.0016260 |
| inclination: | 70.9991° |
| perigee height: | 830 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 72.7233° |
| argument of perigee: | 298.3181° |
| revolutions per day: | 14.14969028 |
| mean anomaly at epoch: | 61.6301° |
| orbit number at epoch: | 81506 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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