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 26105.84883133 +.00000000 +00000-0 +33207-4 0 00005
2 32376 97.8883 290.3493 0001384 91.5326 268.6046 14.82151454 05
| Epoch (UTC): | 15 April 2026 20:22:19 |
| Eccentricity: | 0.0001384 |
| inclination: | 97.8883° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 290.3493° |
| argument of perigee: | 91.5326° |
| revolutions per day: | 14.82151454 |
| mean anomaly at epoch: | 268.6046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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