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 67505U 26145.57251140 +.00000000 +00000-0 +54756-3 0 00009
2 67505 43.0011 239.8986 0001294 274.9455 85.1249 15.27584684 00
| Epoch (UTC): | 25 May 2026 13:44:24 |
| Eccentricity: | 0.0001294 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.8986° |
| argument of perigee: | 274.9455° |
| revolutions per day: | 15.27584684 |
| mean anomaly at epoch: | 85.1249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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