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 07371U 74055 A 75266.95997238 .02312075 +10170-1 +38865-3 0 03466
2 07371 097.3409 263.5078 0008263 289.7037 070.3314 16.34383627067956
| Epoch (UTC): | 23 September 1975 23:02:21 |
| Eccentricity: | 0.0008263 |
| inclination: | 97.3409° |
| perigee height: | 175 km |
| apogee height: | 186 km |
| right ascension of ascending node: | 263.5078° |
| argument of perigee: | 289.7037° |
| revolutions per day: | 16.34383627 |
| mean anomaly at epoch: | 70.3314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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