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 12389U 81033B 15063.84594419 .00103068 17737-5 78462-3 0 9995
2 12389 082.8644 211.7052 0126785 241.3372 280.7539 15.61961392749968
| Epoch (UTC): | 04 March 2015 20:18:09 |
| Eccentricity: | 0.0126785 |
| inclination: | 82.8644° |
| perigee height: | 296 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 211.7052° |
| argument of perigee: | 241.3372° |
| revolutions per day: | 15.61961392 |
| mean anomaly at epoch: | 280.7539° |
| orbit number at epoch: | 74996 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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