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 55465U 26145.58222676 +.00000000 +00000-0 +66169-4 0 00006
2 55465 43.0034 254.3058 0001447 275.0156 85.0531 15.27564655 08
| Epoch (UTC): | 25 May 2026 13:58:24 |
| Eccentricity: | 0.0001447 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.3058° |
| argument of perigee: | 275.0156° |
| revolutions per day: | 15.27564655 |
| mean anomaly at epoch: | 85.0531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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