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 55478U 26145.32212219 +.00000000 +00000-0 +12633-3 0 00000
2 55478 43.0013 245.3471 0001420 274.6020 85.4669 15.27595630 07
| Epoch (UTC): | 25 May 2026 07:43:51 |
| Eccentricity: | 0.0001420 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.3471° |
| argument of perigee: | 274.6020° |
| revolutions per day: | 15.27595630 |
| mean anomaly at epoch: | 85.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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