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 64204U 26145.43872630 +.00000000 +00000-0 +46286-3 0 00009
2 64204 53.1602 43.3020 0002310 87.9915 272.1350 15.30206842 03
| Epoch (UTC): | 25 May 2026 10:31:45 |
| Eccentricity: | 0.0002310 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 43.3020° |
| argument of perigee: | 87.9915° |
| revolutions per day: | 15.30206842 |
| mean anomaly at epoch: | 272.1350° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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