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 57114U 26145.18016554 +.00000000 +00000-0 +22010-4 0 00008
2 57114 43.0013 209.3249 0002244 320.2403 39.8283 15.26742875 06
| Epoch (UTC): | 25 May 2026 04:19:26 |
| Eccentricity: | 0.0002244 |
| inclination: | 43.0013° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 209.3249° |
| argument of perigee: | 320.2403° |
| revolutions per day: | 15.26742875 |
| mean anomaly at epoch: | 39.8283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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