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 26162.44754698 +.00000000 +00000-0 -94362-4 0 00005
2 22285 71.0199 167.4408 0004276 197.4318 162.6659 14.15463805 02
| Epoch (UTC): | 11 June 2026 10:44:28 |
| Eccentricity: | 0.0004276 |
| inclination: | 71.0199° |
| perigee height: | 838 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 167.4408° |
| argument of perigee: | 197.4318° |
| revolutions per day: | 14.15463805 |
| mean anomaly at epoch: | 162.6659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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