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 00043U 60006 A 74037.77776050 .00988543 +09018-2 +01753-4 0 09299
2 00043 033.0454 016.0357 0002584 233.4948 126.5498 16.39800644771946
| Epoch (UTC): | 06 February 1974 18:39:58 |
| Eccentricity: | 0.0002584 |
| inclination: | 33.0454° |
| perigee height: | 165 km |
| apogee height: | 168 km |
| right ascension of ascending node: | 16.0357° |
| argument of perigee: | 233.4948° |
| revolutions per day: | 16.39800644 |
| mean anomaly at epoch: | 126.5498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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