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 64726U 26145.37641712 +.00000000 +00000-0 +59133-3 0 00001
2 64726 53.1593 184.7911 0001730 92.5698 267.5501 15.30215078 02
| Epoch (UTC): | 25 May 2026 09:02:02 |
| Eccentricity: | 0.0001730 |
| inclination: | 53.1593° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.7911° |
| argument of perigee: | 92.5698° |
| revolutions per day: | 15.30215078 |
| mean anomaly at epoch: | 267.5501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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