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 66465U 26145.51716553 +.00000000 +00000-0 +97256-3 0 00003
2 66465 43.0003 222.5081 0002065 279.3588 80.7030 15.27588321 04
| Epoch (UTC): | 25 May 2026 12:24:43 |
| Eccentricity: | 0.0002065 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 222.5081° |
| argument of perigee: | 279.3588° |
| revolutions per day: | 15.27588321 |
| mean anomaly at epoch: | 80.7030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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