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 00837U 64040 B 69337.00000000 .00000000 +00000-0 +00000-0 0 00283
2 00837 037.6659 173.3149 4104709 050.3309 267.4881 00.24013709004713
| Epoch (UTC): | 03 December 1969 00:00:00 |
| Eccentricity: | 0.4104709 |
| inclination: | 37.6659° |
| perigee height: | 58078 km |
| apogee height: | 147835 km |
| right ascension of ascending node: | 173.3149° |
| argument of perigee: | 50.3309° |
| revolutions per day: | 0.24013709 |
| mean anomaly at epoch: | 267.4881° |
| orbit number at epoch: | 471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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