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 26075.61294822 +.00000000 +00000-0 +83787-4 0 00005
2 26931 67.0495 123.7073 0006976 264.9535 95.0771 14.31915665 09
| Epoch (UTC): | 16 March 2026 14:42:38 |
| Eccentricity: | 0.0006976 |
| inclination: | 67.0495° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 123.7073° |
| argument of perigee: | 264.9535° |
| revolutions per day: | 14.31915665 |
| mean anomaly at epoch: | 95.0771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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