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 32276U 26140.53591588 +.00000000 +00000-0 +00000-0 0 00000
2 32276 65.6091 316.9910 0008143 336.0455 203.0511 2.13103103 06
| Epoch (UTC): | 20 May 2026 12:51:43 |
| Eccentricity: | 0.0008143 |
| inclination: | 65.6091° |
| perigee height: | 19109 km |
| apogee height: | 19151 km |
| right ascension of ascending node: | 316.9910° |
| argument of perigee: | 336.0455° |
| revolutions per day: | 2.13103103 |
| mean anomaly at epoch: | 203.0511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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