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 03052U 67117 A 67337.13958417 .00204410 +00000-0 +00000-0 0 9997
2 03052 065.6450 188.8038 0096850 044.2525 316.6232 16.05291380001238
| Epoch (UTC): | 03 December 1967 03:21:00 |
| Eccentricity: | 0.0096850 |
| inclination: | 65.6450° |
| perigee height: | 195 km |
| apogee height: | 324 km |
| right ascension of ascending node: | 188.8038° |
| argument of perigee: | 44.2525° |
| revolutions per day: | 16.05291380 |
| mean anomaly at epoch: | 316.6232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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