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 26626U 26149.68299220 +.00000000 +00000-0 +00000-0 0 00005
2 26626 59.7132 277.2028 0007439 277.8447 82.0345 1.58823457 06
| Epoch (UTC): | 29 May 2026 16:23:30 |
| Eccentricity: | 0.0007439 |
| inclination: | 59.7132° |
| perigee height: | 24630 km |
| apogee height: | 24676 km |
| right ascension of ascending node: | 277.2028° |
| argument of perigee: | 277.8447° |
| revolutions per day: | 1.58823457 |
| mean anomaly at epoch: | 82.0345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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