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 25578U 98074B 13142.50309339 .00000116 00000-0 34529-4 0 4112
2 25578 086.3967 157.0489 0002516 105.6836 004.9595 14.34218947764311
| Epoch (UTC): | 22 May 2013 12:04:27 |
| Eccentricity: | 0.0002516 |
| inclination: | 86.3967° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 157.0489° |
| argument of perigee: | 105.6836° |
| revolutions per day: | 14.34218947 |
| mean anomaly at epoch: | 4.9595° |
| orbit number at epoch: | 76431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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