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 26040.25940374 +.00000000 +00000-0 -40248-5 0 00002
2 22285 71.0200 63.9503 0005157 323.6081 36.4690 14.15440987 09
| Epoch (UTC): | 09 February 2026 06:13:32 |
| Eccentricity: | 0.0005157 |
| inclination: | 71.0200° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 63.9503° |
| argument of perigee: | 323.6081° |
| revolutions per day: | 14.15440987 |
| mean anomaly at epoch: | 36.4690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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