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 57643U 26145.35272053 +.00000000 +00000-0 +83873-4 0 00006
2 57643 43.0063 19.3705 0001476 270.5873 89.4810 15.27588774 02
| Epoch (UTC): | 25 May 2026 08:27:55 |
| Eccentricity: | 0.0001476 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.3705° |
| argument of perigee: | 270.5873° |
| revolutions per day: | 15.27588774 |
| mean anomaly at epoch: | 89.4810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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