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 25193.62402614 -.00000212 00000-0 -84787-4 0 9994
2 20625 70.9997 82.0762 0016217 304.3381 55.6207 14.14970759814434
| Epoch (UTC): | 12 July 2025 14:58:35 |
| Eccentricity: | 0.0016217 |
| inclination: | 70.9997° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 82.0762° |
| argument of perigee: | 304.3381° |
| revolutions per day: | 14.14970759 |
| mean anomaly at epoch: | 55.6207° |
| orbit number at epoch: | 81443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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