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 55467U 26145.57452199 +.00000000 +00000-0 +10103-4 0 00009
2 55467 43.0025 254.2504 0001722 272.7248 87.3406 15.27572293 00
| Epoch (UTC): | 25 May 2026 13:47:18 |
| Eccentricity: | 0.0001722 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.2504° |
| argument of perigee: | 272.7248° |
| revolutions per day: | 15.27572293 |
| mean anomaly at epoch: | 87.3406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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