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 04487U 70059 A 70274.97406788 .03868936 +00000-0 +00000-0 0 9996
2 04487 081.9240 223.8424 0046000 235.9575 123.7288 16.28221562008239
| Epoch (UTC): | 01 October 1970 23:22:39 |
| Eccentricity: | 0.0046000 |
| inclination: | 81.9240° |
| perigee height: | 167 km |
| apogee height: | 227 km |
| right ascension of ascending node: | 223.8424° |
| argument of perigee: | 235.9575° |
| revolutions per day: | 16.28221562 |
| mean anomaly at epoch: | 123.7288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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