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 26106.75992954 +.00000000 +00000-0 -15005-5 0 00004
2 22285 71.0199 284.3456 0006388 255.0414 105.0003 14.15453446 02
| Epoch (UTC): | 16 April 2026 18:14:17 |
| Eccentricity: | 0.0006388 |
| inclination: | 71.0199° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 284.3456° |
| argument of perigee: | 255.0414° |
| revolutions per day: | 14.15453446 |
| mean anomaly at epoch: | 105.0003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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