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 57931U 26145.36685494 +.00000000 +00000-0 -20368-3 0 00004
2 57931 43.0036 255.6691 0000838 253.0971 106.9789 15.27608685 01
| Epoch (UTC): | 25 May 2026 08:48:16 |
| Eccentricity: | 0.0000838 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.6691° |
| argument of perigee: | 253.0971° |
| revolutions per day: | 15.27608685 |
| mean anomaly at epoch: | 106.9789° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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