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 63054U 26144.77478971 +.00000000 +00000-0 +15432-2 0 00005
2 63054 43.0009 277.0315 0001175 41.8416 318.2541 15.70957792 05
| Epoch (UTC): | 24 May 2026 18:35:41 |
| Eccentricity: | 0.0001175 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 277.0315° |
| argument of perigee: | 41.8416° |
| revolutions per day: | 15.70957792 |
| mean anomaly at epoch: | 318.2541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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