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 57330U 26145.48790473 +.00000000 +00000-0 +21185-4 0 00002
2 57330 43.0032 178.5224 0001872 281.7698 78.2943 15.27576263 07
| Epoch (UTC): | 25 May 2026 11:42:34 |
| Eccentricity: | 0.0001872 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.5224° |
| argument of perigee: | 281.7698° |
| revolutions per day: | 15.27576263 |
| mean anomaly at epoch: | 78.2943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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