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 63005U 26145.21710675 +.00000000 +00000-0 +14535-2 0 00004
2 63005 43.0025 93.6997 0003531 261.3168 98.7299 15.70983288 07
| Epoch (UTC): | 25 May 2026 05:12:38 |
| Eccentricity: | 0.0003531 |
| inclination: | 43.0025° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 93.6997° |
| argument of perigee: | 261.3168° |
| revolutions per day: | 15.70983288 |
| mean anomaly at epoch: | 98.7299° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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