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 66089U 26145.61426233 +.00000000 +00000-0 +36368-3 0 00006
2 66089 53.1605 106.4530 0001652 98.6180 261.5008 15.30203918 00
| Epoch (UTC): | 25 May 2026 14:44:32 |
| Eccentricity: | 0.0001652 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.4530° |
| argument of perigee: | 98.6180° |
| revolutions per day: | 15.30203918 |
| mean anomaly at epoch: | 261.5008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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