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 00670U 26106.09139245 +.00000000 +00000-0 +12438-3 0 00005
2 00670 89.9669 333.1375 0040411 210.0607 149.8221 13.44674001 00
| Epoch (UTC): | 16 April 2026 02:11:36 |
| Eccentricity: | 0.0040411 |
| inclination: | 89.9669° |
| perigee height: | 1062 km |
| apogee height: | 1122 km |
| right ascension of ascending node: | 333.1375° |
| argument of perigee: | 210.0607° |
| revolutions per day: | 13.44674001 |
| mean anomaly at epoch: | 149.8221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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