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 65756U 26144.85801403 +.00000000 +00000-0 +75043-3 0 00000
2 65756 53.1622 339.2102 0000939 88.7794 271.3315 15.30214639 00
| Epoch (UTC): | 24 May 2026 20:35:32 |
| Eccentricity: | 0.0000939 |
| inclination: | 53.1622° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 339.2102° |
| argument of perigee: | 88.7794° |
| revolutions per day: | 15.30214639 |
| mean anomaly at epoch: | 271.3315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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