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 32956U 26104.18578000 +.00000000 +00000-0 -28995-3 0 00007
2 32956 82.5091 37.5729 0021975 93.5516 266.8078 12.43068808 05
| Epoch (UTC): | 14 April 2026 04:27:31 |
| Eccentricity: | 0.0021975 |
| inclination: | 82.5091° |
| perigee height: | 1476 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 37.5729° |
| argument of perigee: | 93.5516° |
| revolutions per day: | 12.43068808 |
| mean anomaly at epoch: | 266.8078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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