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 26152.06233976 +.00000000 +00000-0 +78297-3 0 00009
2 39132 64.8477 166.2173 0018476 287.9299 71.9849 15.91707673 08
| Epoch (UTC): | 01 June 2026 01:29:46 |
| Eccentricity: | 0.0018476 |
| inclination: | 64.8477° |
| perigee height: | 285 km |
| apogee height: | 310 km |
| right ascension of ascending node: | 166.2173° |
| argument of perigee: | 287.9299° |
| revolutions per day: | 15.91707673 |
| mean anomaly at epoch: | 71.9849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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