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 57404U 26145.47938192 +.00000000 +00000-0 +43449-4 0 00002
2 57404 43.0032 174.9357 0001972 279.3931 80.6697 15.27578192 06
| Epoch (UTC): | 25 May 2026 11:30:18 |
| Eccentricity: | 0.0001972 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.9357° |
| argument of perigee: | 279.3931° |
| revolutions per day: | 15.27578192 |
| mean anomaly at epoch: | 80.6697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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