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 26106.90992227 +.00000000 +00000-0 +13861-3 0 00003
2 00670 89.9667 333.1347 0040477 207.6553 152.2442 13.44674149 07
| Epoch (UTC): | 16 April 2026 21:50:17 |
| Eccentricity: | 0.0040477 |
| inclination: | 89.9667° |
| perigee height: | 1062 km |
| apogee height: | 1122 km |
| right ascension of ascending node: | 333.1347° |
| argument of perigee: | 207.6553° |
| revolutions per day: | 13.44674149 |
| mean anomaly at epoch: | 152.2442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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