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 00065U 60017 A 60336.92132948 .03564668 +00000-0 +00000-0 0 00057
2 00065 065.0000 216.0710 0035092 066.5949 293.5926 16.29251414000101
| Epoch (UTC): | 01 December 1960 22:06:42 |
| Eccentricity: | 0.0035092 |
| inclination: | 65.0000° |
| perigee height: | 171 km |
| apogee height: | 217 km |
| right ascension of ascending node: | 216.0710° |
| argument of perigee: | 66.5949° |
| revolutions per day: | 16.29251414 |
| mean anomaly at epoch: | 293.5926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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