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 67635U 26145.11735446 +.00000000 +00000-0 +59534-3 0 00008
2 67635 43.0039 68.0327 0001477 260.4795 99.5889 15.27606384 06
| Epoch (UTC): | 25 May 2026 02:48:59 |
| Eccentricity: | 0.0001477 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 68.0327° |
| argument of perigee: | 260.4795° |
| revolutions per day: | 15.27606384 |
| mean anomaly at epoch: | 99.5889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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