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 04039U 69059 A 69197.57294666 .00299999 +00000-0 +00000-0 0 00013
2 04039 032.5111 359.6217 0997319 183.1454 275.7502 16.32730510000004
| Epoch (UTC): | 16 July 1969 13:45:02 |
| Eccentricity: | 0.0997319 |
| inclination: | 32.5111° |
| perigee height: | -469 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 359.6217° |
| argument of perigee: | 183.1454° |
| revolutions per day: | 16.32730510 |
| mean anomaly at epoch: | 275.7502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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