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 21610U 91050F 13142.15071796 .00000314 00000-0 11465-3 0 2173
2 21610 098.7620 153.1341 0004056 068.8215 330.8336 14.39904678146038
| Epoch (UTC): | 22 May 2013 03:37:02 |
| Eccentricity: | 0.0004056 |
| inclination: | 98.7620° |
| perigee height: | 756 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 153.1341° |
| argument of perigee: | 68.8215° |
| revolutions per day: | 14.39904678 |
| mean anomaly at epoch: | 330.8336° |
| orbit number at epoch: | 14603 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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