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 55813U 26145.40850340 +.00000000 +00000-0 +32330-3 0 00001
2 55813 87.9149 309.5172 0001347 89.8806 270.2481 13.19726228 08
| Epoch (UTC): | 25 May 2026 09:48:14 |
| Eccentricity: | 0.0001347 |
| inclination: | 87.9149° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5172° |
| argument of perigee: | 89.8806° |
| revolutions per day: | 13.19726228 |
| mean anomaly at epoch: | 270.2481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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