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 66471U 26145.62352303 +.00000000 +00000-0 +52216-3 0 00008
2 66471 42.9991 221.5810 0001451 268.9049 91.1637 15.27592466 02
| Epoch (UTC): | 25 May 2026 14:57:52 |
| Eccentricity: | 0.0001451 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.5810° |
| argument of perigee: | 268.9049° |
| revolutions per day: | 15.27592466 |
| mean anomaly at epoch: | 91.1637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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