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 64895U 26145.58796604 +.00000000 +00000-0 +31081-3 0 00004
2 64895 97.4561 114.0337 0005116 252.7838 107.2843 15.29077507 01
| Epoch (UTC): | 25 May 2026 14:06:40 |
| Eccentricity: | 0.0005116 |
| inclination: | 97.4561° |
| perigee height: | 475 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 114.0337° |
| argument of perigee: | 252.7838° |
| revolutions per day: | 15.29077507 |
| mean anomaly at epoch: | 107.2843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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