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 58143U 26145.43157704 +.00000000 +00000-0 +18228-3 0 00007
2 58143 34.9922 150.7688 0002390 39.8905 320.1983 15.17461004 00
| Epoch (UTC): | 25 May 2026 10:21:28 |
| Eccentricity: | 0.0002390 |
| inclination: | 34.9922° |
| perigee height: | 512 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 150.7688° |
| argument of perigee: | 39.8905° |
| revolutions per day: | 15.17461004 |
| mean anomaly at epoch: | 320.1983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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