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 57994U 26145.30980852 +.00000000 +00000-0 +33718-5 0 00007
2 57994 43.0055 354.4157 0001722 303.9930 56.0758 15.27562764 07
| Epoch (UTC): | 25 May 2026 07:26:07 |
| Eccentricity: | 0.0001722 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.4157° |
| argument of perigee: | 303.9930° |
| revolutions per day: | 15.27562764 |
| mean anomaly at epoch: | 56.0758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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