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 26138.39119244 +.00000000 +00000-0 +22301-3 0 00005
2 20691 63.2951 292.1819 0881578 84.6092 285.4758 13.62578994 07
| Epoch (UTC): | 18 May 2026 09:23:19 |
| Eccentricity: | 0.0881578 |
| inclination: | 63.2951° |
| perigee height: | 374 km |
| apogee height: | 1679 km |
| right ascension of ascending node: | 292.1819° |
| argument of perigee: | 84.6092° |
| revolutions per day: | 13.62578994 |
| mean anomaly at epoch: | 285.4758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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