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 12399U 81034 A 81104.42585921 .00095709 +31152-5 +15153-3 0 9995
2 12399 040.3358 249.3707 0009190 248.0645 111.7494 16.02948953000317
| Epoch (UTC): | 14 April 1981 10:13:14 |
| Eccentricity: | 0.0009190 |
| inclination: | 40.3358° |
| perigee height: | 260 km |
| apogee height: | 272 km |
| right ascension of ascending node: | 249.3707° |
| argument of perigee: | 248.0645° |
| revolutions per day: | 16.02948953 |
| mean anomaly at epoch: | 111.7494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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