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 66530U 26145.59633244 +.00000000 +00000-0 +29153-3 0 00000
2 66530 42.9996 203.7540 0001386 277.7383 82.3311 15.27594752 02
| Epoch (UTC): | 25 May 2026 14:18:43 |
| Eccentricity: | 0.0001386 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 203.7540° |
| argument of perigee: | 277.7383° |
| revolutions per day: | 15.27594752 |
| mean anomaly at epoch: | 82.3311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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