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 66561U 26144.75562374 +.00000000 +00000-0 +57430-3 0 00005
2 66561 43.0035 277.4367 0001999 272.2753 87.7870 15.27582451 00
| Epoch (UTC): | 24 May 2026 18:08:05 |
| Eccentricity: | 0.0001999 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.4367° |
| argument of perigee: | 272.2753° |
| revolutions per day: | 15.27582451 |
| mean anomaly at epoch: | 87.7870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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