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 15891U 85059 A 85197.89068985 .00062907 +00000-0 +46079-4 0 00102
2 15891 082.3543 355.4398 0043293 076.4179 284.1335 16.13353075001093
| Epoch (UTC): | 16 July 1985 21:22:35 |
| Eccentricity: | 0.0043293 |
| inclination: | 82.3543° |
| perigee height: | 209 km |
| apogee height: | 266 km |
| right ascension of ascending node: | 355.4398° |
| argument of perigee: | 76.4179° |
| revolutions per day: | 16.13353075 |
| mean anomaly at epoch: | 284.1335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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