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 67165U 26145.54987448 +.00000000 +00000-0 +37767-3 0 00008
2 67165 43.0004 236.3307 0001234 274.3893 85.6818 15.27585280 07
| Epoch (UTC): | 25 May 2026 13:11:49 |
| Eccentricity: | 0.0001234 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.3307° |
| argument of perigee: | 274.3893° |
| revolutions per day: | 15.27585280 |
| mean anomaly at epoch: | 85.6818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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