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 data is extracted from the following two-line orbital elements,
1 20580U 90037B 13139.12107178 .00002055 00000-0 13452-3 0 2429
2 20580 028.4701 103.3684 0003540 041.6360 020.5257 15.03600057 65319
| Epoch (UTC): | 19 May 2013 02:54:20 |
| Eccentricity: | 0.0003540 |
| inclination: | 28.4701° |
| perigee height: | 553 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 103.3684° |
| argument of perigee: | 41.6360° |
| revolutions per day: | 15.03600057 |
| mean anomaly at epoch: | 20.5257° |
| orbit number at epoch: | 6531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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