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 20625U 26022.46468212 +.00000000 +00000-0 -46199-4 0 00007
2 20625 70.9994 34.9929 0013895 4.1270 355.9965 14.15007922 04
| Epoch (UTC): | 22 January 2026 11:09:08 |
| Eccentricity: | 0.0013895 |
| inclination: | 70.9994° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 34.9929° |
| argument of perigee: | 4.1270° |
| revolutions per day: | 14.15007922 |
| mean anomaly at epoch: | 355.9965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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