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 26100.26895279 +.00000000 +00000-0 +96235-4 0 00000
2 26931 67.0508 59.9347 0006777 264.4977 95.5352 14.31929669 01
| Epoch (UTC): | 10 April 2026 06:27:17 |
| Eccentricity: | 0.0006777 |
| inclination: | 67.0508° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 59.9347° |
| argument of perigee: | 264.4977° |
| revolutions per day: | 14.31929669 |
| mean anomaly at epoch: | 95.5352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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