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 55483U 26145.36549464 +.00000000 +00000-0 +12377-4 0 00001
2 55483 43.0013 266.5565 0001343 270.7399 89.3298 15.27576081 02
| Epoch (UTC): | 25 May 2026 08:46:18 |
| Eccentricity: | 0.0001343 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5565° |
| argument of perigee: | 270.7399° |
| revolutions per day: | 15.27576081 |
| mean anomaly at epoch: | 89.3298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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