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 63183U 26145.59973039 +.00000000 +00000-0 +11988-2 0 00006
2 63183 43.0004 216.6195 0000836 49.0712 311.0228 15.70928276 08
| Epoch (UTC): | 25 May 2026 14:23:36 |
| Eccentricity: | 0.0000836 |
| inclination: | 43.0004° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 216.6195° |
| argument of perigee: | 49.0712° |
| revolutions per day: | 15.70928276 |
| mean anomaly at epoch: | 311.0228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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