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 57328U 26145.47637104 +.00000000 +00000-0 -11002-3 0 00006
2 57328 43.0036 178.4380 0001860 293.6081 66.4575 15.27549835 00
| Epoch (UTC): | 25 May 2026 11:25:58 |
| Eccentricity: | 0.0001860 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.4380° |
| argument of perigee: | 293.6081° |
| revolutions per day: | 15.27549835 |
| mean anomaly at epoch: | 66.4575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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