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 66474U 26145.55428160 +.00000000 +00000-0 +44831-3 0 00002
2 66474 42.9989 221.9204 0001027 272.5393 87.5341 15.27588925 01
| Epoch (UTC): | 25 May 2026 13:18:09 |
| Eccentricity: | 0.0001027 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 221.9204° |
| argument of perigee: | 272.5393° |
| revolutions per day: | 15.27588925 |
| mean anomaly at epoch: | 87.5341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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