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 56112U 26144.84000395 +.00000000 +00000-0 -49512-4 0 00000
2 56112 43.0060 91.8446 0001393 283.3136 76.7560 15.26727019 05
| Epoch (UTC): | 24 May 2026 20:09:36 |
| Eccentricity: | 0.0001393 |
| inclination: | 43.0060° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 91.8446° |
| argument of perigee: | 283.3136° |
| revolutions per day: | 15.26727019 |
| mean anomaly at epoch: | 76.7560° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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