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 57347U 26145.56564490 +.00000000 +00000-0 +11737-4 0 00009
2 57347 43.0015 181.6551 0000892 265.0800 94.9950 15.27581442 03
| Epoch (UTC): | 25 May 2026 13:34:31 |
| Eccentricity: | 0.0000892 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 181.6551° |
| argument of perigee: | 265.0800° |
| revolutions per day: | 15.27581442 |
| mean anomaly at epoch: | 94.9950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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