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 26474U 26075.85222469 +.00000000 +00000-0 +24101-3 0 00005
2 26474 67.9909 20.3679 0038805 26.8845 333.4303 15.09636547 04
| Epoch (UTC): | 16 March 2026 20:27:12 |
| Eccentricity: | 0.0038805 |
| inclination: | 67.9909° |
| perigee height: | 510 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 20.3679° |
| argument of perigee: | 26.8845° |
| revolutions per day: | 15.09636547 |
| mean anomaly at epoch: | 333.4303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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