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 67836U 26145.46436954 +.00000000 +00000-0 +36576-3 0 00002
2 67836 43.0019 193.6487 0001524 284.3299 75.7383 15.27602220 06
| Epoch (UTC): | 25 May 2026 11:08:41 |
| Eccentricity: | 0.0001524 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.6487° |
| argument of perigee: | 284.3299° |
| revolutions per day: | 15.27602220 |
| mean anomaly at epoch: | 75.7383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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