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 57443U 26145.12804616 +.00000000 +00000-0 +47404-4 0 00005
2 57443 43.0003 188.0315 0001267 264.7239 95.3468 15.27579310 05
| Epoch (UTC): | 25 May 2026 03:04:23 |
| Eccentricity: | 0.0001267 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.0315° |
| argument of perigee: | 264.7239° |
| revolutions per day: | 15.27579310 |
| mean anomaly at epoch: | 95.3468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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