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 67849U 26145.48364713 +.00000000 +00000-0 +16146-2 0 00001
2 67849 42.9995 193.7936 0001631 264.6769 95.3896 15.27644959 05
| Epoch (UTC): | 25 May 2026 11:36:27 |
| Eccentricity: | 0.0001631 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.7936° |
| argument of perigee: | 264.6769° |
| revolutions per day: | 15.27644959 |
| mean anomaly at epoch: | 95.3896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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