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 04225U 69099 A 69318.67491029 .01999999 +00000-0 +00000-0 0 9996
2 04225 032.5565 159.6900 0000010 273.0803 086.9196 16.32726311000006
| Epoch (UTC): | 14 November 1969 16:11:52 |
| Eccentricity: | 0.0000010 |
| inclination: | 32.5565° |
| perigee height: | 185 km |
| apogee height: | 185 km |
| right ascension of ascending node: | 159.6900° |
| argument of perigee: | 273.0803° |
| revolutions per day: | 16.32726311 |
| mean anomaly at epoch: | 86.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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