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 05598U 71096 A 87061.32870574 .15942513 -16120-3 +82295-3 0 9991
2 05598 003.6018 120.7082 0328775 222.3022 134.2839 15.72733572058197
| Epoch (UTC): | 02 March 1987 07:53:20 |
| Eccentricity: | 0.0328775 |
| inclination: | 3.6018° |
| perigee height: | 130 km |
| apogee height: | 572 km |
| right ascension of ascending node: | 120.7082° |
| argument of perigee: | 222.3022° |
| revolutions per day: | 15.72733572 |
| mean anomaly at epoch: | 134.2839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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