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 57354U 26145.35472111 +.00000000 +00000-0 +47491-4 0 00008
2 57354 43.0003 168.7630 0001206 272.8682 87.2032 15.27581930 04
| Epoch (UTC): | 25 May 2026 08:30:47 |
| Eccentricity: | 0.0001206 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.7630° |
| argument of perigee: | 272.8682° |
| revolutions per day: | 15.27581930 |
| mean anomaly at epoch: | 87.2032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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