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 57407U 26145.42093933 +.00000000 +00000-0 +15176-4 0 00001
2 57407 43.0044 160.7294 0001836 277.6489 82.4155 15.27576114 04
| Epoch (UTC): | 25 May 2026 10:06:09 |
| Eccentricity: | 0.0001836 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 160.7294° |
| argument of perigee: | 277.6489° |
| revolutions per day: | 15.27576114 |
| mean anomaly at epoch: | 82.4155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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