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 01516U 65068 A 65238.35371715 .00465042 +57804-3 +00000-0 0 9992
2 01516 032.6144 007.2850 0072683 119.3144 241.4289 16.09722886000779
| Epoch (UTC): | 26 August 1965 08:29:21 |
| Eccentricity: | 0.0072683 |
| inclination: | 32.6144° |
| perigee height: | 199 km |
| apogee height: | 296 km |
| right ascension of ascending node: | 7.2850° |
| argument of perigee: | 119.3144° |
| revolutions per day: | 16.09722886 |
| mean anomaly at epoch: | 241.4289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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