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 66002U 26145.56959625 +.00000000 +00000-0 +42578-4 0 00002
2 66002 50.0064 256.7109 0000944 153.3625 206.7296 13.29325359 07
| Epoch (UTC): | 25 May 2026 13:40:13 |
| Eccentricity: | 0.0000944 |
| inclination: | 50.0064° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 256.7109° |
| argument of perigee: | 153.3625° |
| revolutions per day: | 13.29325359 |
| mean anomaly at epoch: | 206.7296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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