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 26070.86332469 +.00000000 +00000-0 +86947-4 0 00008
2 26931 67.0503 135.9916 0007010 265.1305 94.8997 14.31913406 06
| Epoch (UTC): | 11 March 2026 20:43:11 |
| Eccentricity: | 0.0007010 |
| inclination: | 67.0503° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 135.9916° |
| argument of perigee: | 265.1305° |
| revolutions per day: | 14.31913406 |
| mean anomaly at epoch: | 94.8997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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