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 22626U 26111.55872505 +.00000000 +00000-0 +11462-3 0 00006
2 22626 82.5201 225.7054 0016944 156.8685 203.3303 14.96728897 01
| Epoch (UTC): | 21 April 2026 13:24:33 |
| Eccentricity: | 0.0016944 |
| inclination: | 82.5201° |
| perigee height: | 565 km |
| apogee height: | 589 km |
| right ascension of ascending node: | 225.7054° |
| argument of perigee: | 156.8685° |
| revolutions per day: | 14.96728897 |
| mean anomaly at epoch: | 203.3303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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