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 39422U 26118.90039424 +.00000000 +00000-0 +27031-3 0 00008
2 39422 97.6179 89.6198 0009111 182.2148 177.9038 15.02467037 00
| Epoch (UTC): | 28 April 2026 21:36:34 |
| Eccentricity: | 0.0009111 |
| inclination: | 97.6179° |
| perigee height: | 553 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 89.6198° |
| argument of perigee: | 182.2148° |
| revolutions per day: | 15.02467037 |
| mean anomaly at epoch: | 177.9038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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