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 66750U 26145.44481861 +.00000000 +00000-0 +17977-3 0 00005
2 66750 97.4234 219.5410 0002804 55.9202 304.2298 15.19644620 00
| Epoch (UTC): | 25 May 2026 10:40:32 |
| Eccentricity: | 0.0002804 |
| inclination: | 97.4234° |
| perigee height: | 505 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 219.5410° |
| argument of perigee: | 55.9202° |
| revolutions per day: | 15.19644620 |
| mean anomaly at epoch: | 304.2298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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