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 55932U 26145.50218747 +.00000000 +00000-0 -28992-3 0 00003
2 55932 70.0018 70.5984 0002656 265.8614 94.2241 14.98326093 03
| Epoch (UTC): | 25 May 2026 12:03:08 |
| Eccentricity: | 0.0002656 |
| inclination: | 70.0018° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.5984° |
| argument of perigee: | 265.8614° |
| revolutions per day: | 14.98326093 |
| mean anomaly at epoch: | 94.2241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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