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 03663U 69006 A 84093.51187641 .10820157 -10215-4 +42885-3 0 9994
2 03663 032.9414 151.2549 0001682 309.5448 051.5905 16.44327629845837
| Epoch (UTC): | 02 April 1984 12:17:06 |
| Eccentricity: | 0.0001682 |
| inclination: | 32.9414° |
| perigee height: | 153 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 151.2549° |
| argument of perigee: | 309.5448° |
| revolutions per day: | 16.44327629 |
| mean anomaly at epoch: | 51.5905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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