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 57050U 26145.12610921 +.00000000 +00000-0 -88769-5 0 00004
2 57050 43.0030 38.8770 0000903 227.8597 132.2178 15.27578683 00
| Epoch (UTC): | 25 May 2026 03:01:35 |
| Eccentricity: | 0.0000903 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 38.8770° |
| argument of perigee: | 227.8597° |
| revolutions per day: | 15.27578683 |
| mean anomaly at epoch: | 132.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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