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 57417U 26145.54733469 +.00000000 +00000-0 +83296-4 0 00008
2 57417 43.0024 174.5781 0001542 266.5208 93.5468 15.27589817 01
| Epoch (UTC): | 25 May 2026 13:08:09 |
| Eccentricity: | 0.0001542 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.5781° |
| argument of perigee: | 266.5208° |
| revolutions per day: | 15.27589817 |
| mean anomaly at epoch: | 93.5468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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