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 20691U 90050C 25188.06454532 .00006953 00000-0 52028-3 0 9998
2 20691 63.2973 60.5900 0889981 78.5568 291.3963 13.59423662 59325
| Epoch (UTC): | 07 July 2025 01:32:56 |
| Eccentricity: | 0.0889981 |
| inclination: | 63.2973° |
| perigee height: | 378 km |
| apogee height: | 1698 km |
| right ascension of ascending node: | 60.5900° |
| argument of perigee: | 78.5568° |
| revolutions per day: | 13.59423662 |
| mean anomaly at epoch: | 291.3963° |
| orbit number at epoch: | 5932 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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