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 26088.10310324 +.00000000 +00000-0 +11828-3 0 00003
2 22285 71.0230 323.5146 0006506 274.8622 85.1758 14.15454721 04
| Epoch (UTC): | 29 March 2026 02:28:28 |
| Eccentricity: | 0.0006506 |
| inclination: | 71.0230° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 323.5146° |
| argument of perigee: | 274.8622° |
| revolutions per day: | 14.15454721 |
| mean anomaly at epoch: | 85.1758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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