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 55432U 26145.42537556 +.00000000 +00000-0 +12236-4 0 00005
2 55432 69.9989 270.9452 0003375 264.1543 95.9231 14.98327122 01
| Epoch (UTC): | 25 May 2026 10:12:32 |
| Eccentricity: | 0.0003375 |
| inclination: | 69.9989° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 270.9452° |
| argument of perigee: | 264.1543° |
| revolutions per day: | 14.98327122 |
| mean anomaly at epoch: | 95.9231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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