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 20580U 26112.19370843 +.00000000 +00000-0 +15003-3 0 00007
2 20580 28.4737 103.0742 0001772 237.2093 122.8332 15.30106155 06
| Epoch (UTC): | 22 April 2026 04:38:56 |
| Eccentricity: | 0.0001772 |
| inclination: | 28.4737° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 103.0742° |
| argument of perigee: | 237.2093° |
| revolutions per day: | 15.30106155 |
| mean anomaly at epoch: | 122.8332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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