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 26108.52667734 +.00000000 +00000-0 +49548-4 0 00003
2 22285 71.0198 280.6361 0006314 253.1273 106.9158 14.15453679 05
| Epoch (UTC): | 18 April 2026 12:38:24 |
| Eccentricity: | 0.0006314 |
| inclination: | 71.0198° |
| perigee height: | 836 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 280.6361° |
| argument of perigee: | 253.1273° |
| revolutions per day: | 14.15453679 |
| mean anomaly at epoch: | 106.9158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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