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 63265U 26145.33127969 +.00000000 +00000-0 +15890-2 0 00008
2 63265 43.0006 10.2204 0001589 281.8653 78.2036 15.70900211 04
| Epoch (UTC): | 25 May 2026 07:57:02 |
| Eccentricity: | 0.0001589 |
| inclination: | 43.0006° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 10.2204° |
| argument of perigee: | 281.8653° |
| revolutions per day: | 15.70900211 |
| mean anomaly at epoch: | 78.2036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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