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 data is extracted from the following two-line orbital elements,
1 00692U 63039C 68084.10555552 -.00000374 +00000-0 +00000-0 0 00000
2 00692 036.7283 179.1791 0852721 237.5470 072.7561 00.22091344003596
| Epoch (UTC): | 24 March 1968 02:32:00 |
| Eccentricity: | 0.0852721 |
| inclination: | 36.7283° |
| perigee height: | 99355 km |
| apogee height: | 119068 km |
| right ascension of ascending node: | 179.1791° |
| argument of perigee: | 237.5470° |
| revolutions per day: | 0.22091344 |
| mean anomaly at epoch: | 72.7561° |
| orbit number at epoch: | 359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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