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 26037.50325411 +.00000000 +00000-0 -61228-4 0 00005
2 22285 71.0202 69.7371 0005098 326.2555 33.8243 14.15441314 07
| Epoch (UTC): | 06 February 2026 12:04:41 |
| Eccentricity: | 0.0005098 |
| inclination: | 71.0202° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 69.7371° |
| argument of perigee: | 326.2555° |
| revolutions per day: | 14.15441314 |
| mean anomaly at epoch: | 33.8243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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