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 64016U 26145.42346456 +.00000000 +00000-0 -17039-3 0 00006
2 64016 43.0001 284.3473 0001540 279.2027 80.8650 15.27576491 01
| Epoch (UTC): | 25 May 2026 10:09:47 |
| Eccentricity: | 0.0001540 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 284.3473° |
| argument of perigee: | 279.2027° |
| revolutions per day: | 15.27576491 |
| mean anomaly at epoch: | 80.8650° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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