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 66422U 26145.54937029 +.00000000 +00000-0 +76768-3 0 00007
2 66422 43.0011 200.4982 0001934 266.6734 93.3896 15.27593661 00
| Epoch (UTC): | 25 May 2026 13:11:05 |
| Eccentricity: | 0.0001934 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.4982° |
| argument of perigee: | 266.6734° |
| revolutions per day: | 15.27593661 |
| mean anomaly at epoch: | 93.3896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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