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 00740U 64004 A 69156.79556806 .03889016 +00000-0 +00000-0 0 9993
2 00740 081.3964 155.7916 0041610 159.4828 200.7969 15.24081695264654
| Epoch (UTC): | 05 June 1969 19:05:37 |
| Eccentricity: | 0.0041610 |
| inclination: | 81.3964° |
| perigee height: | 465 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 155.7916° |
| argument of perigee: | 159.4828° |
| revolutions per day: | 15.24081695 |
| mean anomaly at epoch: | 200.7969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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