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 63309U 26145.39667523 +.00000000 +00000-0 +12847-2 0 00007
2 63309 43.0001 161.9863 0001315 281.1483 78.9237 15.70860652 08
| Epoch (UTC): | 25 May 2026 09:31:12 |
| Eccentricity: | 0.0001315 |
| inclination: | 43.0001° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 161.9863° |
| argument of perigee: | 281.1483° |
| revolutions per day: | 15.70860652 |
| mean anomaly at epoch: | 78.9237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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