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 32376U 26039.82351975 +.00000000 +00000-0 +89566-4 0 00002
2 32376 97.8843 225.2805 0001516 82.1796 277.9589 14.82157089 04
| Epoch (UTC): | 08 February 2026 19:45:52 |
| Eccentricity: | 0.0001516 |
| inclination: | 97.8843° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 225.2805° |
| argument of perigee: | 82.1796° |
| revolutions per day: | 14.82157089 |
| mean anomaly at epoch: | 277.9589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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