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 26934U 01044A 13141.07381724 0.00019000 00000-0 24257-3 0 01
2 26934 97.0285 273.0526 0001889 246.2510 113.7489 15.59266141 01
| Epoch (UTC): | 21 May 2013 01:46:17 |
| Eccentricity: | 0.0001889 |
| inclination: | 97.0285° |
| perigee height: | 388 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 273.0526° |
| argument of perigee: | 246.2510° |
| revolutions per day: | 15.59266141 |
| mean anomaly at epoch: | 113.7489° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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