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 57071U 26145.03824279 +.00000000 +00000-0 +50499-5 0 00008
2 57071 43.0054 25.2303 0001220 265.9662 94.1050 15.27573947 03
| Epoch (UTC): | 25 May 2026 00:55:04 |
| Eccentricity: | 0.0001220 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.2303° |
| argument of perigee: | 265.9662° |
| revolutions per day: | 15.27573947 |
| mean anomaly at epoch: | 94.1050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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