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 66043U 26145.43119968 +.00000000 +00000-0 +94639-4 0 00006
2 66043 89.0021 43.1784 0013530 211.4258 148.6129 14.26793311 01
| Epoch (UTC): | 25 May 2026 10:20:55 |
| Eccentricity: | 0.0013530 |
| inclination: | 89.0021° |
| perigee height: | 793 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 43.1784° |
| argument of perigee: | 211.4258° |
| revolutions per day: | 14.26793311 |
| mean anomaly at epoch: | 148.6129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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