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 16230U 85104 A 85310.20833356 .00050804 +00000-0 +25592-3 0 9990
2 16230 056.9883 164.5370 0007752 319.3127 348.8615 15.81311631000999
| Epoch (UTC): | 06 November 1985 05:00:00 |
| Eccentricity: | 0.0007752 |
| inclination: | 56.9883° |
| perigee height: | 321 km |
| apogee height: | 332 km |
| right ascension of ascending node: | 164.5370° |
| argument of perigee: | 319.3127° |
| revolutions per day: | 15.81311631 |
| mean anomaly at epoch: | 348.8615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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