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 55934U 26145.27726045 +.00000000 +00000-0 +22599-4 0 00001
2 55934 70.0000 91.2995 0003321 269.3843 90.6936 14.98334249 04
| Epoch (UTC): | 25 May 2026 06:39:15 |
| Eccentricity: | 0.0003321 |
| inclination: | 70.0000° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2995° |
| argument of perigee: | 269.3843° |
| revolutions per day: | 14.98334249 |
| mean anomaly at epoch: | 90.6936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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