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 22006U 26106.97709124 +.00000000 +00000-0 +37109-4 0 00001
2 22006 82.9303 103.5713 0038446 85.2978 303.7958 13.75186203 02
| Epoch (UTC): | 16 April 2026 23:27:00 |
| Eccentricity: | 0.0038446 |
| inclination: | 82.9303° |
| perigee height: | 953 km |
| apogee height: | 1009 km |
| right ascension of ascending node: | 103.5713° |
| argument of perigee: | 85.2978° |
| revolutions per day: | 13.75186203 |
| mean anomaly at epoch: | 303.7958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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