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 13162.05416784 0.00016000 00000-0 19884-3 0 04
2 26934 97.0285 293.8472 0003000 67.7150 292.2848 15.59974496 05
| Epoch (UTC): | 11 June 2013 01:18:00 |
| Eccentricity: | 0.0003000 |
| inclination: | 97.0285° |
| perigee height: | 386 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 293.8472° |
| argument of perigee: | 67.7150° |
| revolutions per day: | 15.59974496 |
| mean anomaly at epoch: | 292.2848° |
| 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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