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 19884U 89021C 14067.65752520 .00017183 00000-0 17591-2 0 9041
2 19884 026.3734 199.6509 6116582 210.0221 021.7203 03.89911772285617
| Epoch (UTC): | 08 March 2014 15:46:50 |
| Eccentricity: | 0.6116582 |
| inclination: | 26.3734° |
| perigee height: | 243 km |
| apogee height: | 21102 km |
| right ascension of ascending node: | 199.6509° |
| argument of perigee: | 210.0221° |
| revolutions per day: | 3.89911772 |
| mean anomaly at epoch: | 21.7203° |
| orbit number at epoch: | 28561 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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