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 54126U 26145.37216705 +.00000000 +00000-0 +60234-4 0 00009
2 54126 87.9149 309.5240 0001426 84.2259 275.9036 13.19726661 08
| Epoch (UTC): | 25 May 2026 08:55:55 |
| Eccentricity: | 0.0001426 |
| inclination: | 87.9149° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5240° |
| argument of perigee: | 84.2259° |
| revolutions per day: | 13.19726661 |
| mean anomaly at epoch: | 275.9036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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