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 20508U 26160.20146397 +.00000000 +00000-0 +31567-4 0 00001
2 20508 82.9562 79.9043 0045378 101.4440 9.3133 13.74556319 05
| Epoch (UTC): | 09 June 2026 04:50:06 |
| Eccentricity: | 0.0045378 |
| inclination: | 82.9562° |
| perigee height: | 950 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 79.9043° |
| argument of perigee: | 101.4440° |
| revolutions per day: | 13.74556319 |
| mean anomaly at epoch: | 9.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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