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 66850U 26145.64844293 +.00000000 +00000-0 +10332-2 0 00007
2 66850 43.0000 269.0038 0001307 284.2424 75.8283 15.27613754 03
| Epoch (UTC): | 25 May 2026 15:33:45 |
| Eccentricity: | 0.0001307 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.0038° |
| argument of perigee: | 284.2424° |
| revolutions per day: | 15.27613754 |
| mean anomaly at epoch: | 75.8283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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