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 66090U 26145.59843358 +.00000000 +00000-0 +67516-3 0 00005
2 66090 53.1582 106.3540 0001663 92.7819 267.3372 15.30202938 01
| Epoch (UTC): | 25 May 2026 14:21:44 |
| Eccentricity: | 0.0001663 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.3540° |
| argument of perigee: | 92.7819° |
| revolutions per day: | 15.30202938 |
| mean anomaly at epoch: | 267.3372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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