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 63009U 26145.24365937 +.00000000 +00000-0 +17496-2 0 00007
2 63009 43.0000 93.9088 0001641 263.0878 96.9803 15.70906025 00
| Epoch (UTC): | 25 May 2026 05:50:52 |
| Eccentricity: | 0.0001641 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 93.9088° |
| argument of perigee: | 263.0878° |
| revolutions per day: | 15.70906025 |
| mean anomaly at epoch: | 96.9803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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