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 00877U 64053B 13138.07461276 .00000168 00000-0 60010-4 0 2886
2 00877 065.0795 327.2780 0076446 324.6705 034.9340 14.58556026583976
| Epoch (UTC): | 18 May 2013 01:47:26 |
| Eccentricity: | 0.0076446 |
| inclination: | 65.0795° |
| perigee height: | 644 km |
| apogee height: | 752 km |
| right ascension of ascending node: | 327.2780° |
| argument of perigee: | 324.6705° |
| revolutions per day: | 14.58556026 |
| mean anomaly at epoch: | 34.9340° |
| orbit number at epoch: | 58397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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