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 63268U 26144.99212366 +.00000000 +00000-0 +13044-2 0 00007
2 63268 43.0026 11.9654 0002260 277.4221 82.6390 15.70890890 08
| Epoch (UTC): | 24 May 2026 23:48:39 |
| Eccentricity: | 0.0002260 |
| inclination: | 43.0026° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 11.9654° |
| argument of perigee: | 277.4221° |
| revolutions per day: | 15.70890890 |
| mean anomaly at epoch: | 82.6390° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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