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 54124U 26145.35480138 +.00000000 +00000-0 +79905-5 0 00004
2 54124 87.9159 309.5136 0001701 85.2285 274.9042 13.19725723 01
| Epoch (UTC): | 25 May 2026 08:30:54 |
| Eccentricity: | 0.0001701 |
| inclination: | 87.9159° |
| perigee height: | 1184 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5136° |
| argument of perigee: | 85.2285° |
| revolutions per day: | 13.19725723 |
| mean anomaly at epoch: | 274.9042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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