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 28773U 05025A 13145.13623490 .00003520 00000-0 23384-3 0 254
2 28773 031.3829 138.5443 0006320 303.5594 135.7383 15.05487483432625
| Epoch (UTC): | 25 May 2013 03:16:10 |
| Eccentricity: | 0.0006320 |
| inclination: | 31.3829° |
| perigee height: | 545 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 138.5443° |
| argument of perigee: | 303.5594° |
| revolutions per day: | 15.05487483 |
| mean anomaly at epoch: | 135.7383° |
| orbit number at epoch: | 43262 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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