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 55461U 26145.00659971 +.00000000 +00000-0 -12485-4 0 00004
2 55461 42.9988 257.7323 0001334 266.1062 93.9637 15.27584372 07
| Epoch (UTC): | 25 May 2026 00:09:30 |
| Eccentricity: | 0.0001334 |
| inclination: | 42.9988° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 257.7323° |
| argument of perigee: | 266.1062° |
| revolutions per day: | 15.27584372 |
| mean anomaly at epoch: | 93.9637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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