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 00255U 62006 A 81281.45891398 .13376733 -72757-5 +28507-3 0 9995
2 00255 032.8099 205.8817 0000050 093.5650 268.1215 16.47262862082941
| Epoch (UTC): | 08 October 1981 11:00:50 |
| Eccentricity: | 0.0000050 |
| inclination: | 32.8099° |
| perigee height: | 146 km |
| apogee height: | 146 km |
| right ascension of ascending node: | 205.8817° |
| argument of perigee: | 93.5650° |
| revolutions per day: | 16.47262862 |
| mean anomaly at epoch: | 268.1215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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