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 63329U 26145.49896720 +.00000000 +00000-0 +84364-3 0 00007
2 63329 42.9995 317.1387 0001594 264.7007 95.3663 15.27580099 06
| Epoch (UTC): | 25 May 2026 11:58:30 |
| Eccentricity: | 0.0001594 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.1387° |
| argument of perigee: | 264.7007° |
| revolutions per day: | 15.27580099 |
| mean anomaly at epoch: | 95.3663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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