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 19216U 88051B 96340.36293920 .64194205 34729-4 46505-3 0 3848
2 19216 56.9100 66.0967 1385719 63.2476 313.9974 13.38919575 33595
| Epoch (UTC): | 05 December 1996 08:42:37 |
| Eccentricity: | 0.1385719 |
| inclination: | 56.9100° |
| perigee height: | 75 km |
| apogee height: | 2151 km |
| right ascension of ascending node: | 66.0967° |
| argument of perigee: | 63.2476° |
| revolutions per day: | 13.38919575 |
| mean anomaly at epoch: | 313.9974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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