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 04258U 69082 DB 89259.14217888 .28693406 +19000-5 +40781-1 0 9990
2 04258 070.0490 264.0373 0005410 210.9580 151.3417 16.05332824004135
| Epoch (UTC): | 16 September 1989 03:24:44 |
| Eccentricity: | 0.0005410 |
| inclination: | 70.0490° |
| perigee height: | 256 km |
| apogee height: | 263 km |
| right ascension of ascending node: | 264.0373° |
| argument of perigee: | 210.9580° |
| revolutions per day: | 16.05332824 |
| mean anomaly at epoch: | 151.3417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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