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 66464U 26145.60039669 +.00000000 +00000-0 +32548-3 0 00001
2 66464 43.0008 221.4063 0000509 204.2070 155.8758 15.27592726 05
| Epoch (UTC): | 25 May 2026 14:24:34 |
| Eccentricity: | 0.0000509 |
| inclination: | 43.0008° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 221.4063° |
| argument of perigee: | 204.2070° |
| revolutions per day: | 15.27592726 |
| mean anomaly at epoch: | 155.8758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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