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 22237U 92080B 13145.86763024 .00000331 00000-0 43108-4 0 308
2 22237 082.5141 056.9276 0020098 018.4265 047.9320 14.77579948104336
| Epoch (UTC): | 25 May 2013 20:49:23 |
| Eccentricity: | 0.0020098 |
| inclination: | 82.5141° |
| perigee height: | 623 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 56.9276° |
| argument of perigee: | 18.4265° |
| revolutions per day: | 14.77579948 |
| mean anomaly at epoch: | 47.9320° |
| orbit number at epoch: | 10433 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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