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 26906U 26109.80510965 +.00000000 +00000-0 +45255-4 0 00003
2 26906 63.4209 308.2100 0622834 341.7006 16.2474 13.45197072 02
| Epoch (UTC): | 19 April 2026 19:19:21 |
| Eccentricity: | 0.0622834 |
| inclination: | 63.4209° |
| perigee height: | 625 km |
| apogee height: | 1555 km |
| right ascension of ascending node: | 308.2100° |
| argument of perigee: | 341.7006° |
| revolutions per day: | 13.45197072 |
| mean anomaly at epoch: | 16.2474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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