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 22627U 26105.15294183 +.00000000 +00000-0 +20352-4 0 00005
2 22627 82.5234 343.8126 0021607 218.6731 141.2936 14.80121871 05
| Epoch (UTC): | 15 April 2026 03:40:14 |
| Eccentricity: | 0.0021607 |
| inclination: | 82.5234° |
| perigee height: | 614 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 343.8126° |
| argument of perigee: | 218.6731° |
| revolutions per day: | 14.80121871 |
| mean anomaly at epoch: | 141.2936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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