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 55614U 26145.34880441 +.00000000 +00000-0 +72259-4 0 00003
2 55614 43.0031 266.5152 0001548 266.2072 93.8602 15.27580009 09
| Epoch (UTC): | 25 May 2026 08:22:16 |
| Eccentricity: | 0.0001548 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.5152° |
| argument of perigee: | 266.2072° |
| revolutions per day: | 15.27580009 |
| mean anomaly at epoch: | 93.8602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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