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 57827U 26145.41709809 +.00000000 +00000-0 +52428-4 0 00003
2 57827 43.0034 160.7905 0001328 271.1208 88.9491 15.27577271 01
| Epoch (UTC): | 25 May 2026 10:00:37 |
| Eccentricity: | 0.0001328 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.7905° |
| argument of perigee: | 271.1208° |
| revolutions per day: | 15.27577271 |
| mean anomaly at epoch: | 88.9491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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