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 55912U 26145.25374764 +.00000000 +00000-0 +00000-0 0 00001
2 55912 1.0185 358.3040 0004307 339.1099 144.9852 1.00269287 08
| Epoch (UTC): | 25 May 2026 06:05:23 |
| Eccentricity: | 0.0004307 |
| inclination: | 1.0185° |
| perigee height: | 35769 km |
| apogee height: | 35805 km |
| right ascension of ascending node: | 358.3040° |
| argument of perigee: | 339.1099° |
| revolutions per day: | 1.00269287 |
| mean anomaly at epoch: | 144.9852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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