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 25196.94664002 -.00000271 00000-0 -11526-3 0 9998
2 20625 70.9993 75.0987 0016256 299.8213 60.1292 14.14969510814906
| Epoch (UTC): | 15 July 2025 22:43:09 |
| Eccentricity: | 0.0016256 |
| inclination: | 70.9993° |
| perigee height: | 830 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 75.0987° |
| argument of perigee: | 299.8213° |
| revolutions per day: | 14.14969510 |
| mean anomaly at epoch: | 60.1292° |
| orbit number at epoch: | 81490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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