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 67510U 26145.56351160 +.00000000 +00000-0 +56137-3 0 00002
2 67510 43.0003 239.8080 0001052 256.7469 103.3266 15.27587841 07
| Epoch (UTC): | 25 May 2026 13:31:27 |
| Eccentricity: | 0.0001052 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.8080° |
| argument of perigee: | 256.7469° |
| revolutions per day: | 15.27587841 |
| mean anomaly at epoch: | 103.3266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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