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 57432U 26145.48146612 +.00000000 +00000-0 +60368-4 0 00001
2 57432 43.0003 189.8032 0001267 276.7172 83.3536 15.27584161 00
| Epoch (UTC): | 25 May 2026 11:33:18 |
| Eccentricity: | 0.0001267 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.8032° |
| argument of perigee: | 276.7172° |
| revolutions per day: | 15.27584161 |
| mean anomaly at epoch: | 83.3536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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