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 26154.60928777 +.00000000 +00000-0 +91734-4 0 00006
2 26931 67.0512 279.3895 0006115 263.9670 96.0735 14.31950876 07
| Epoch (UTC): | 03 June 2026 14:37:22 |
| Eccentricity: | 0.0006115 |
| inclination: | 67.0512° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 279.3895° |
| argument of perigee: | 263.9670° |
| revolutions per day: | 14.31950876 |
| mean anomaly at epoch: | 96.0735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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