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 59033U 26145.49475090 +.00000000 +00000-0 +70674-4 0 00007
2 59033 43.0017 309.8919 0001153 271.5303 88.5417 15.27571355 01
| Epoch (UTC): | 25 May 2026 11:52:26 |
| Eccentricity: | 0.0001153 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8919° |
| argument of perigee: | 271.5303° |
| revolutions per day: | 15.27571355 |
| mean anomaly at epoch: | 88.5417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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