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 26112.49210590 +.00000000 +00000-0 +62555-4 0 00003
2 26931 67.0527 28.3222 0006562 264.1709 95.8645 14.31933477 06
| Epoch (UTC): | 22 April 2026 11:48:37 |
| Eccentricity: | 0.0006562 |
| inclination: | 67.0527° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 28.3222° |
| argument of perigee: | 264.1709° |
| revolutions per day: | 14.31933477 |
| mean anomaly at epoch: | 95.8645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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