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 57509U 26145.43403888 +.00000000 +00000-0 +59656-4 0 00000
2 57509 43.0047 302.5370 0002421 255.4147 104.6436 15.27579681 08
| Epoch (UTC): | 25 May 2026 10:25:00 |
| Eccentricity: | 0.0002421 |
| inclination: | 43.0047° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 302.5370° |
| argument of perigee: | 255.4147° |
| revolutions per day: | 15.27579681 |
| mean anomaly at epoch: | 104.6436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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