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 57144U 26145.17370190 +.00000000 +00000-0 +16398-4 0 00001
2 57144 43.0032 191.1438 0001244 273.9307 86.1402 15.27577027 08
| Epoch (UTC): | 25 May 2026 04:10:07 |
| Eccentricity: | 0.0001244 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 191.1438° |
| argument of perigee: | 273.9307° |
| revolutions per day: | 15.27577027 |
| mean anomaly at epoch: | 86.1402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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