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 39413U 98067DB 14059.46000733 .24423758 13053-4 20830-3 0 9999
2 39413 051.7296 265.3968 0033589 042.8845 321.3539 16.48564713 15816
| Epoch (UTC): | 28 February 2014 11:02:24 |
| Eccentricity: | 0.0033589 |
| inclination: | 51.7296° |
| perigee height: | 121 km |
| apogee height: | 165 km |
| right ascension of ascending node: | 265.3968° |
| argument of perigee: | 42.8845° |
| revolutions per day: | 16.48564713 |
| mean anomaly at epoch: | 321.3539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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