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 64052U 26145.62019340 +.00000000 +00000-0 +43465-3 0 00008
2 64052 97.3751 218.4547 0001732 214.7517 145.3607 15.23374785 03
| Epoch (UTC): | 25 May 2026 14:53:04 |
| Eccentricity: | 0.0001732 |
| inclination: | 97.3751° |
| perigee height: | 494 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 218.4547° |
| argument of perigee: | 214.7517° |
| revolutions per day: | 15.23374785 |
| mean anomaly at epoch: | 145.3607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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