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 55335U 26145.53806645 +.00000000 +00000-0 +92786-6 0 00007
2 55335 42.9990 229.6442 0001180 262.3995 97.6722 15.27573138 06
| Epoch (UTC): | 25 May 2026 12:54:48 |
| Eccentricity: | 0.0001180 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.6442° |
| argument of perigee: | 262.3995° |
| revolutions per day: | 15.27573138 |
| mean anomaly at epoch: | 97.6722° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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