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 66669U 26145.61752387 +.00000000 +00000-0 +10181-2 0 00006
2 66669 97.4076 220.0115 0008309 99.1868 261.0310 15.26013008 09
| Epoch (UTC): | 25 May 2026 14:49:14 |
| Eccentricity: | 0.0008309 |
| inclination: | 97.4076° |
| perigee height: | 482 km |
| apogee height: | 493 km |
| right ascension of ascending node: | 220.0115° |
| argument of perigee: | 99.1868° |
| revolutions per day: | 15.26013008 |
| mean anomaly at epoch: | 261.0310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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