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 00085U 61004C 13143.14301929 .00013165 00000-0 36208-2 0 7923
2 00085 038.7665 079.5774 0479136 056.9373 307.6447 13.95625558565660
| Epoch (UTC): | 23 May 2013 03:25:56 |
| Eccentricity: | 0.0479136 |
| inclination: | 38.7665° |
| perigee height: | 560 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 79.5774° |
| argument of perigee: | 56.9373° |
| revolutions per day: | 13.95625558 |
| mean anomaly at epoch: | 307.6447° |
| orbit number at epoch: | 56566 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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