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 66476U 26145.50559789 +.00000000 +00000-0 +51721-3 0 00007
2 66476 42.9988 222.4131 0001218 277.6739 82.3974 15.27598057 01
| Epoch (UTC): | 25 May 2026 12:08:03 |
| Eccentricity: | 0.0001218 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.4131° |
| argument of perigee: | 277.6739° |
| revolutions per day: | 15.27598057 |
| mean anomaly at epoch: | 82.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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