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 55480U 26145.36933782 +.00000000 +00000-0 +19543-4 0 00000
2 55480 43.0015 266.5002 0001358 271.9031 88.1665 15.27576108 04
| Epoch (UTC): | 25 May 2026 08:51:50 |
| Eccentricity: | 0.0001358 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5002° |
| argument of perigee: | 271.9031° |
| revolutions per day: | 15.27576108 |
| mean anomaly at epoch: | 88.1665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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