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 26137.50121875 +.00000000 +00000-0 -61029-4 0 00003
2 22285 71.0215 219.8092 0005602 224.0250 136.0427 14.15458199 06
| Epoch (UTC): | 17 May 2026 12:01:45 |
| Eccentricity: | 0.0005602 |
| inclination: | 71.0215° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 219.8092° |
| argument of perigee: | 224.0250° |
| revolutions per day: | 14.15458199 |
| mean anomaly at epoch: | 136.0427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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