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 02947U 67088 A 67266.18014044 .00269981 +00000-0 +00000-0 0 9995
2 02947 051.7898 058.9990 0050342 055.0495 305.5140 16.16001374001125
| Epoch (UTC): | 23 September 1967 04:19:24 |
| Eccentricity: | 0.0050342 |
| inclination: | 51.7898° |
| perigee height: | 197 km |
| apogee height: | 264 km |
| right ascension of ascending node: | 58.9990° |
| argument of perigee: | 55.0495° |
| revolutions per day: | 16.16001374 |
| mean anomaly at epoch: | 305.5140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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