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 57131U 26145.56474698 +.00000000 +00000-0 +11335-3 0 00003
2 57131 43.0014 188.9207 0001468 328.1476 31.9286 15.27591355 08
| Epoch (UTC): | 25 May 2026 13:33:14 |
| Eccentricity: | 0.0001468 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.9207° |
| argument of perigee: | 328.1476° |
| revolutions per day: | 15.27591355 |
| mean anomaly at epoch: | 31.9286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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