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 55142U 26145.36957243 +.00000000 +00000-0 -26804-3 0 00001
2 55142 87.8916 25.5960 0001661 86.3760 273.7558 13.11415170 00
| Epoch (UTC): | 25 May 2026 08:52:11 |
| Eccentricity: | 0.0001661 |
| inclination: | 87.8916° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.5960° |
| argument of perigee: | 86.3760° |
| revolutions per day: | 13.11415170 |
| mean anomaly at epoch: | 273.7558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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