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 67519U 26145.56993013 +.00000000 +00000-0 +10311-2 0 00003
2 67519 43.0001 239.8636 0001424 256.2598 103.8095 15.27627748 08
| Epoch (UTC): | 25 May 2026 13:40:41 |
| Eccentricity: | 0.0001424 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.8636° |
| argument of perigee: | 256.2598° |
| revolutions per day: | 15.27627748 |
| mean anomaly at epoch: | 103.8095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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