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 55337U 26145.55653814 +.00000000 +00000-0 +10831-4 0 00008
2 55337 43.0019 215.0200 0001058 267.7572 92.3158 15.27576627 08
| Epoch (UTC): | 25 May 2026 13:21:24 |
| Eccentricity: | 0.0001058 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 215.0200° |
| argument of perigee: | 267.7572° |
| revolutions per day: | 15.27576627 |
| mean anomaly at epoch: | 92.3158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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