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 67833U 26145.43866684 +.00000000 +00000-0 +48622-3 0 00008
2 67833 43.0014 193.4437 0001507 261.6110 98.4571 15.27577859 02
| Epoch (UTC): | 25 May 2026 10:31:40 |
| Eccentricity: | 0.0001507 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.4437° |
| argument of perigee: | 261.6110° |
| revolutions per day: | 15.27577859 |
| mean anomaly at epoch: | 98.4571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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