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 59083U 26145.51042645 +.00000000 +00000-0 +53229-4 0 00008
2 59083 43.0004 153.6729 0001267 274.2296 85.8410 15.27582124 02
| Epoch (UTC): | 25 May 2026 12:15:00 |
| Eccentricity: | 0.0001267 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.6729° |
| argument of perigee: | 274.2296° |
| revolutions per day: | 15.27582124 |
| mean anomaly at epoch: | 85.8410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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