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 01467U 65060 A 69216.02852346 .04443300 +00000-0 +00000-0 0 9997
2 01467 028.8967 102.9535 0000010 257.0464 103.0107 16.35133354224402
| Epoch (UTC): | 04 August 1969 00:41:04 |
| Eccentricity: | 0.0000010 |
| inclination: | 28.8967° |
| perigee height: | 179 km |
| apogee height: | 179 km |
| right ascension of ascending node: | 102.9535° |
| argument of perigee: | 257.0464° |
| revolutions per day: | 16.35133354 |
| mean anomaly at epoch: | 103.0107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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