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 63902U 26145.26663596 +.00000000 +00000-0 +53154-3 0 00005
2 63902 43.0018 103.3704 0001231 275.7734 84.2977 15.27593156 09
| Epoch (UTC): | 25 May 2026 06:23:57 |
| Eccentricity: | 0.0001231 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.3704° |
| argument of perigee: | 275.7734° |
| revolutions per day: | 15.27593156 |
| mean anomaly at epoch: | 84.2977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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