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 26106.31522155 +.00000000 +00000-0 +51108-4 0 00006
2 20508 82.9525 119.7251 0042610 251.6364 118.9764 13.74552082 07
| Epoch (UTC): | 16 April 2026 07:33:55 |
| Eccentricity: | 0.0042610 |
| inclination: | 82.9525° |
| perigee height: | 952 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 119.7251° |
| argument of perigee: | 251.6364° |
| revolutions per day: | 13.74552082 |
| mean anomaly at epoch: | 118.9764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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