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 57178U 26145.55826421 +.00000000 +00000-0 +43022-3 0 00006
2 57178 97.5104 210.8694 0011559 165.3744 194.7833 15.30545950 09
| Epoch (UTC): | 25 May 2026 13:23:54 |
| Eccentricity: | 0.0011559 |
| inclination: | 97.5104° |
| perigee height: | 466 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 210.8694° |
| argument of perigee: | 165.3744° |
| revolutions per day: | 15.30545950 |
| mean anomaly at epoch: | 194.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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