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 04599U 70092 A 70314.34255047 .00181111 +00000-0 +00000-0 0 9993
2 04599 065.4190 177.9333 0052639 064.7266 295.9304 16.13644600001748
| Epoch (UTC): | 10 November 1970 08:13:16 |
| Eccentricity: | 0.0052639 |
| inclination: | 65.4190° |
| perigee height: | 202 km |
| apogee height: | 271 km |
| right ascension of ascending node: | 177.9333° |
| argument of perigee: | 64.7266° |
| revolutions per day: | 16.13644600 |
| mean anomaly at epoch: | 295.9304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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