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 26100.25830089 +.00000000 +00000-0 -83991-4 0 00001
2 22285 71.0207 297.9962 0006597 262.7705 97.2669 14.15454872 08
| Epoch (UTC): | 10 April 2026 06:11:57 |
| Eccentricity: | 0.0006597 |
| inclination: | 71.0207° |
| perigee height: | 836 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 297.9962° |
| argument of perigee: | 262.7705° |
| revolutions per day: | 14.15454872 |
| mean anomaly at epoch: | 97.2669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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