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 57373U 26145.36757701 +.00000000 +00000-0 -25672-4 0 00009
2 57373 43.0016 168.8465 0000676 298.1365 61.9418 15.27563753 05
| Epoch (UTC): | 25 May 2026 08:49:18 |
| Eccentricity: | 0.0000676 |
| inclination: | 43.0016° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.8465° |
| argument of perigee: | 298.1365° |
| revolutions per day: | 15.27563753 |
| mean anomaly at epoch: | 61.9418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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