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 66406U 26145.34644633 +.00000000 +00000-0 +31667-3 0 00002
2 66406 53.1582 219.9761 0001018 94.6724 265.4395 15.34397234 00
| Epoch (UTC): | 25 May 2026 08:18:52 |
| Eccentricity: | 0.0001018 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.9761° |
| argument of perigee: | 94.6724° |
| revolutions per day: | 15.34397234 |
| mean anomaly at epoch: | 265.4395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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