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 22286U 26022.46838784 +.00000000 +00000-0 +33685-3 0 00001
2 22286 82.5181 281.5651 0019596 96.3065 264.0390 14.96960089 00
| Epoch (UTC): | 22 January 2026 11:14:28 |
| Eccentricity: | 0.0019596 |
| inclination: | 82.5181° |
| perigee height: | 563 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 281.5651° |
| argument of perigee: | 96.3065° |
| revolutions per day: | 14.96960089 |
| mean anomaly at epoch: | 264.0390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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