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 57974U 26145.36851499 +.00000000 +00000-0 +54820-4 0 00001
2 57974 43.0035 262.9381 0001646 276.7708 83.2956 15.27580364 08
| Epoch (UTC): | 25 May 2026 08:50:39 |
| Eccentricity: | 0.0001646 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 262.9381° |
| argument of perigee: | 276.7708° |
| revolutions per day: | 15.27580364 |
| mean anomaly at epoch: | 83.2956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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