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 04501U 70065 A 70309.20656273 .04283179 +00000-0 +00000-0 0 9992
2 04501 051.1209 040.7439 0064810 334.9656 024.8175 16.24725342011625
| Epoch (UTC): | 05 November 1970 04:57:27 |
| Eccentricity: | 0.0064810 |
| inclination: | 51.1209° |
| perigee height: | 164 km |
| apogee height: | 249 km |
| right ascension of ascending node: | 40.7439° |
| argument of perigee: | 334.9656° |
| revolutions per day: | 16.24725342 |
| mean anomaly at epoch: | 24.8175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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