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 25142.52053965 .00004425 00000-0 34186-3 0 9991
2 20691 63.2952 182.7261 0890958 77.6738 292.2480 13.58837465 53118
| Epoch (UTC): | 22 May 2025 12:29:34 |
| Eccentricity: | 0.0890958 |
| inclination: | 63.2952° |
| perigee height: | 379 km |
| apogee height: | 1701 km |
| right ascension of ascending node: | 182.7261° |
| argument of perigee: | 77.6738° |
| revolutions per day: | 13.58837465 |
| mean anomaly at epoch: | 292.2480° |
| orbit number at epoch: | 5311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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