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 55156U 26145.41874053 +.00000000 +00000-0 +12191-2 0 00001
2 55156 87.8907 25.6079 0002002 85.3398 274.7958 13.11417558 00
| Epoch (UTC): | 25 May 2026 10:02:59 |
| Eccentricity: | 0.0002002 |
| inclination: | 87.8907° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6079° |
| argument of perigee: | 85.3398° |
| revolutions per day: | 13.11417558 |
| mean anomaly at epoch: | 274.7958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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