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 57200U 26145.63307725 +.00000000 +00000-0 +55593-3 0 00008
2 57200 97.5064 219.2274 0007656 133.0590 227.1300 15.44325714 00
| Epoch (UTC): | 25 May 2026 15:11:37 |
| Eccentricity: | 0.0007656 |
| inclination: | 97.5064° |
| perigee height: | 428 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 219.2274° |
| argument of perigee: | 133.0590° |
| revolutions per day: | 15.44325714 |
| mean anomaly at epoch: | 227.1300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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