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 67107U 26145.24583426 +.00000000 +00000-0 +69229-3 0 00007
2 67107 43.0009 96.7226 0001406 265.0030 95.0661 15.27588311 06
| Epoch (UTC): | 25 May 2026 05:54:00 |
| Eccentricity: | 0.0001406 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.7226° |
| argument of perigee: | 265.0030° |
| revolutions per day: | 15.27588311 |
| mean anomaly at epoch: | 95.0661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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