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 55334U 26145.59571348 +.00000000 +00000-0 +19318-4 0 00009
2 55334 43.0017 229.1197 0001197 276.1975 83.8741 15.27574026 03
| Epoch (UTC): | 25 May 2026 14:17:49 |
| Eccentricity: | 0.0001197 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.1197° |
| argument of perigee: | 276.1975° |
| revolutions per day: | 15.27574026 |
| mean anomaly at epoch: | 83.8741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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