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 67641U 26145.48154402 +.00000000 +00000-0 +58426-3 0 00001
2 67641 43.0004 66.4552 0001659 266.8078 93.2584 15.27608795 04
| Epoch (UTC): | 25 May 2026 11:33:25 |
| Eccentricity: | 0.0001659 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4552° |
| argument of perigee: | 266.8078° |
| revolutions per day: | 15.27608795 |
| mean anomaly at epoch: | 93.2584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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