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 67091U 26145.46536431 +.00000000 +00000-0 +21495-2 0 00009
2 67091 69.9945 169.8339 0006361 286.4248 73.6231 15.35783140 05
| Epoch (UTC): | 25 May 2026 11:10:07 |
| Eccentricity: | 0.0006361 |
| inclination: | 69.9945° |
| perigee height: | 454 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 169.8339° |
| argument of perigee: | 286.4248° |
| revolutions per day: | 15.35783140 |
| mean anomaly at epoch: | 73.6231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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