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 64956U 26145.66611102 +.00000000 +00000-0 +94803-4 0 00002
2 64956 86.4925 290.0419 0001983 91.2487 268.8874 13.24413787 06
| Epoch (UTC): | 25 May 2026 15:59:11 |
| Eccentricity: | 0.0001983 |
| inclination: | 86.4925° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 290.0419° |
| argument of perigee: | 91.2487° |
| revolutions per day: | 13.24413787 |
| mean anomaly at epoch: | 268.8874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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