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 64510U 26145.53727073 +.00000000 +00000-0 +95421-4 0 00006
2 64510 51.8990 230.7353 0000526 109.8486 250.2533 14.79934000 09
| Epoch (UTC): | 25 May 2026 12:53:40 |
| Eccentricity: | 0.0000526 |
| inclination: | 51.8990° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 230.7353° |
| argument of perigee: | 109.8486° |
| revolutions per day: | 14.79934000 |
| mean anomaly at epoch: | 250.2533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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