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 66574U 26145.62492208 +.00000000 +00000-0 +58826-3 0 00004
2 66574 42.9995 272.7803 0001108 258.3593 101.7135 15.27590266 03
| Epoch (UTC): | 25 May 2026 14:59:53 |
| Eccentricity: | 0.0001108 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.7803° |
| argument of perigee: | 258.3593° |
| revolutions per day: | 15.27590266 |
| mean anomaly at epoch: | 101.7135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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