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 66869U 26145.65358913 +.00000000 +00000-0 +60850-3 0 00008
2 66869 42.9996 269.0367 0001027 277.6941 82.3794 15.27600373 02
| Epoch (UTC): | 25 May 2026 15:41:10 |
| Eccentricity: | 0.0001027 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 269.0367° |
| argument of perigee: | 277.6941° |
| revolutions per day: | 15.27600373 |
| mean anomaly at epoch: | 82.3794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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