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 is defined by the following mean orbital elements,
1 20691U 26146.31713950 +.00000000 +00000-0 +28070-3 0 00009
2 20691 63.2952 270.8052 0881249 84.7628 285.3227 13.62636115 01
| Epoch (UTC): | 26 May 2026 07:36:40 |
| Eccentricity: | 0.0881249 |
| inclination: | 63.2952° |
| perigee height: | 374 km |
| apogee height: | 1679 km |
| right ascension of ascending node: | 270.8052° |
| argument of perigee: | 84.7628° |
| revolutions per day: | 13.62636115 |
| mean anomaly at epoch: | 285.3227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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