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 26931U 26106.55514959 +.00000000 +00000-0 +52474-4 0 00008
2 26931 67.0519 43.6767 0006654 264.3453 95.6890 14.31931581 05
| Epoch (UTC): | 16 April 2026 13:19:24 |
| Eccentricity: | 0.0006654 |
| inclination: | 67.0519° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 43.6767° |
| argument of perigee: | 264.3453° |
| revolutions per day: | 14.31931581 |
| mean anomaly at epoch: | 95.6890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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