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 22285U 26039.12867558 +.00000000 +00000-0 -37793-4 0 00008
2 22285 71.0201 66.3244 0005127 324.6897 35.3885 14.15440992 02
| Epoch (UTC): | 08 February 2026 03:05:17 |
| Eccentricity: | 0.0005127 |
| inclination: | 71.0201° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 66.3244° |
| argument of perigee: | 324.6897° |
| revolutions per day: | 14.15440992 |
| mean anomaly at epoch: | 35.3885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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