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 03626U 68118 A 68356.65757754 .00000000 +00000-0 +00000-0 0 00019
2 03626 030.7142 141.9251 9763415 029.5976 000.0393 00.05901781000008
| Epoch (UTC): | 21 December 1968 15:46:54 |
| Eccentricity: | 0.9763415 |
| inclination: | 30.7142° |
| perigee height: | 214 km |
| apogee height: | 544356 km |
| right ascension of ascending node: | 141.9251° |
| argument of perigee: | 29.5976° |
| revolutions per day: | 0.05901781 |
| mean anomaly at epoch: | 0.0393° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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