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 66369U 26145.54668933 +.00000000 +00000-0 +19864-3 0 00006
2 66369 53.1586 233.2287 0001652 88.5712 271.5478 15.30200722 08
| Epoch (UTC): | 25 May 2026 13:07:13 |
| Eccentricity: | 0.0001652 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.2287° |
| argument of perigee: | 88.5712° |
| revolutions per day: | 15.30200722 |
| mean anomaly at epoch: | 271.5478° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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