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 53432U 26145.63732701 +.00000000 +00000-0 +28947-3 0 00000
2 53432 53.2132 118.4486 0001114 83.6192 276.4927 15.08819725 06
| Epoch (UTC): | 25 May 2026 15:17:45 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 118.4486° |
| argument of perigee: | 83.6192° |
| revolutions per day: | 15.08819725 |
| mean anomaly at epoch: | 276.4927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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