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 is defined by the following mean orbital elements,
1 12903U 81103A 15243.25221526 .18772571 -97346-6 19782-3 0 9992
2 12903 081.0885 314.8004 0011558 263.3522 096.7389 16.50252196859203
| Epoch (UTC): | 31 August 2015 06:03:11 |
| Eccentricity: | 0.0011558 |
| inclination: | 81.0885° |
| perigee height: | 131 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 314.8004° |
| argument of perigee: | 263.3522° |
| revolutions per day: | 16.50252196 |
| mean anomaly at epoch: | 96.7389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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