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 57183U 26145.60674600 +.00000000 +00000-0 +20836-3 0 00006
2 57183 97.5103 204.3755 0011313 180.8723 179.2493 15.18747304 00
| Epoch (UTC): | 25 May 2026 14:33:42 |
| Eccentricity: | 0.0011313 |
| inclination: | 97.5103° |
| perigee height: | 502 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 204.3755° |
| argument of perigee: | 180.8723° |
| revolutions per day: | 15.18747304 |
| mean anomaly at epoch: | 179.2493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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