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 64091U 26145.56761028 +.00000000 +00000-0 +58650-3 0 00003
2 64091 97.4673 222.5190 0013523 84.4683 275.8096 15.23758365 08
| Epoch (UTC): | 25 May 2026 13:37:21 |
| Eccentricity: | 0.0013523 |
| inclination: | 97.4673° |
| perigee height: | 485 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 222.5190° |
| argument of perigee: | 84.4683° |
| revolutions per day: | 15.23758365 |
| mean anomaly at epoch: | 275.8096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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