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 55338U 26145.54191360 +.00000000 +00000-0 -20299-4 0 00001
2 55338 43.0020 229.6753 0001346 272.5464 87.5233 15.27579628 03
| Epoch (UTC): | 25 May 2026 13:00:21 |
| Eccentricity: | 0.0001346 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 229.6753° |
| argument of perigee: | 272.5464° |
| revolutions per day: | 15.27579628 |
| mean anomaly at epoch: | 87.5233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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