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 54235U 26145.62773301 +.00000000 +00000-0 +17923-4 0 00005
2 54235 98.8170 153.3584 0001705 132.8524 227.2792 14.13366353 07
| Epoch (UTC): | 25 May 2026 15:03:56 |
| Eccentricity: | 0.0001705 |
| inclination: | 98.8170° |
| perigee height: | 847 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 153.3584° |
| argument of perigee: | 132.8524° |
| revolutions per day: | 14.13366353 |
| mean anomaly at epoch: | 227.2792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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