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 64088U 26145.65012286 +.00000000 +00000-0 +38073-3 0 00001
2 64088 97.4729 221.7247 0009564 93.4642 266.7686 15.18075325 01
| Epoch (UTC): | 25 May 2026 15:36:10 |
| Eccentricity: | 0.0009564 |
| inclination: | 97.4729° |
| perigee height: | 505 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 221.7247° |
| argument of perigee: | 93.4642° |
| revolutions per day: | 15.18075325 |
| mean anomaly at epoch: | 266.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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