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 64503U 26145.57244147 +.00000000 +00000-0 +52166-3 0 00006
2 64503 51.8991 260.5822 0000395 117.6335 242.4668 14.79940499 09
| Epoch (UTC): | 25 May 2026 13:44:18 |
| Eccentricity: | 0.0000395 |
| inclination: | 51.8991° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 260.5822° |
| argument of perigee: | 117.6335° |
| revolutions per day: | 14.79940499 |
| mean anomaly at epoch: | 242.4668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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