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 07122U 74008 A 83022.79673856 .15056995 +00931-5 +02122-4 0 9996
2 07122 031.2190 299.0018 0021974 102.0462 258.4614 16.42308998419461
| Epoch (UTC): | 22 January 1983 19:07:18 |
| Eccentricity: | 0.0021974 |
| inclination: | 31.2190° |
| perigee height: | 145 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 299.0018° |
| argument of perigee: | 102.0462° |
| revolutions per day: | 16.42308998 |
| mean anomaly at epoch: | 258.4614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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