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 26139.87181922 +.00000000 +00000-0 +51158-4 0 00007
2 26931 67.0507 317.5081 0006217 263.5445 96.4949 14.31943954 02
| Epoch (UTC): | 19 May 2026 20:55:25 |
| Eccentricity: | 0.0006217 |
| inclination: | 67.0507° |
| perigee height: | 781 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 317.5081° |
| argument of perigee: | 263.5445° |
| revolutions per day: | 14.31943954 |
| mean anomaly at epoch: | 96.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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