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 64334U 26145.42612355 +.00000000 +00000-0 +76488-3 0 00005
2 64334 42.9955 48.5689 0000929 46.4388 313.6541 15.27576274 08
| Epoch (UTC): | 25 May 2026 10:13:37 |
| Eccentricity: | 0.0000929 |
| inclination: | 42.9955° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5689° |
| argument of perigee: | 46.4388° |
| revolutions per day: | 15.27576274 |
| mean anomaly at epoch: | 313.6541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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