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 55834U 26145.38638931 +.00000000 +00000-0 +49393-5 0 00000
2 55834 87.9150 309.5228 0001738 103.1041 257.0286 13.19725926 00
| Epoch (UTC): | 25 May 2026 09:16:24 |
| Eccentricity: | 0.0001738 |
| inclination: | 87.9150° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5228° |
| argument of perigee: | 103.1041° |
| revolutions per day: | 13.19725926 |
| mean anomaly at epoch: | 257.0286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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