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 57824U 26145.53631873 +.00000000 +00000-0 +25043-4 0 00001
2 57824 43.0009 159.9675 0001108 273.3601 86.7124 15.27570602 01
| Epoch (UTC): | 25 May 2026 12:52:17 |
| Eccentricity: | 0.0001108 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 159.9675° |
| argument of perigee: | 273.3601° |
| revolutions per day: | 15.27570602 |
| mean anomaly at epoch: | 86.7124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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