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 66304U 26145.55838507 +.00000000 +00000-0 +55643-3 0 00007
2 66304 45.4198 236.0830 0012824 291.3606 68.5914 15.26911644 00
| Epoch (UTC): | 25 May 2026 13:24:04 |
| Eccentricity: | 0.0012824 |
| inclination: | 45.4198° |
| perigee height: | 476 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 236.0830° |
| argument of perigee: | 291.3606° |
| revolutions per day: | 15.26911644 |
| mean anomaly at epoch: | 68.5914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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