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 67643U 26145.50708888 +.00000000 +00000-0 +71110-3 0 00004
2 67643 43.0050 65.7998 0001439 267.1430 92.9257 15.27617341 05
| Epoch (UTC): | 25 May 2026 12:10:12 |
| Eccentricity: | 0.0001439 |
| inclination: | 43.0050° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 65.7998° |
| argument of perigee: | 267.1430° |
| revolutions per day: | 15.27617341 |
| mean anomaly at epoch: | 92.9257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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