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 66798U 26145.43598595 +.00000000 +00000-0 +76794-3 0 00001
2 66798 43.0038 41.1877 0001523 264.0531 96.0147 15.27593849 06
| Epoch (UTC): | 25 May 2026 10:27:49 |
| Eccentricity: | 0.0001523 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 41.1877° |
| argument of perigee: | 264.0531° |
| revolutions per day: | 15.27593849 |
| mean anomaly at epoch: | 96.0147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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