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 66014U 26145.28242694 +.00000000 +00000-0 +30180-3 0 00000
2 66014 53.1605 108.0452 0000807 98.7048 261.4044 15.30196604 06
| Epoch (UTC): | 25 May 2026 06:46:41 |
| Eccentricity: | 0.0000807 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.0452° |
| argument of perigee: | 98.7048° |
| revolutions per day: | 15.30196604 |
| mean anomaly at epoch: | 261.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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