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 04368U 70027B 83003.00024306 -.00000501 +00000-0 +10000-3 0 00044
2 04368 057.3500 065.6307 0668113 079.1100 274.6481 00.21467209003593
| Epoch (UTC): | 03 January 1983 00:00:21 |
| Eccentricity: | 0.0668113 |
| inclination: | 57.3500° |
| perigee height: | 103570 km |
| apogee height: | 119313 km |
| right ascension of ascending node: | 65.6307° |
| argument of perigee: | 79.1100° |
| revolutions per day: | 0.21467209 |
| mean anomaly at epoch: | 274.6481° |
| orbit number at epoch: | 359 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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