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 67996U 26145.51590198 +.00000000 +00000-0 +97522-3 0 00004
2 67996 42.9986 334.9962 0000987 77.4353 282.6609 15.27551407 06
| Epoch (UTC): | 25 May 2026 12:22:53 |
| Eccentricity: | 0.0000987 |
| inclination: | 42.9986° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.9962° |
| argument of perigee: | 77.4353° |
| revolutions per day: | 15.27551407 |
| mean anomaly at epoch: | 282.6609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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