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 57334U 26145.44050417 +.00000000 +00000-0 +23728-4 0 00004
2 57334 43.0014 179.0210 0001294 269.4713 90.5991 15.27577041 06
| Epoch (UTC): | 25 May 2026 10:34:19 |
| Eccentricity: | 0.0001294 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 179.0210° |
| argument of perigee: | 269.4713° |
| revolutions per day: | 15.27577041 |
| mean anomaly at epoch: | 90.5991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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