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 26041.53147301 +.00000000 +00000-0 +35976-4 0 00003
2 22285 71.0200 61.2795 0005192 322.4617 37.6143 14.15441096 02
| Epoch (UTC): | 10 February 2026 12:45:19 |
| Eccentricity: | 0.0005192 |
| inclination: | 71.0200° |
| perigee height: | 837 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 61.2795° |
| argument of perigee: | 322.4617° |
| revolutions per day: | 14.15441096 |
| mean anomaly at epoch: | 37.6143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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