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 63328U 26145.49593666 +.00000000 +00000-0 +74620-3 0 00003
2 63328 43.0017 309.3266 0001070 276.1183 83.9547 15.27589545 01
| Epoch (UTC): | 25 May 2026 11:54:08 |
| Eccentricity: | 0.0001070 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.3266° |
| argument of perigee: | 276.1183° |
| revolutions per day: | 15.27589545 |
| mean anomaly at epoch: | 83.9547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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