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 39132U 26107.22355330 +.00000000 +00000-0 +45544-3 0 00005
2 39132 64.8559 326.0970 0016624 269.6014 90.3236 15.77252264 05
| Epoch (UTC): | 17 April 2026 05:21:55 |
| Eccentricity: | 0.0016624 |
| inclination: | 64.8559° |
| perigee height: | 327 km |
| apogee height: | 349 km |
| right ascension of ascending node: | 326.0970° |
| argument of perigee: | 269.6014° |
| revolutions per day: | 15.77252264 |
| mean anomaly at epoch: | 90.3236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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