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 07478U 74080 A 74312.09597253 .00125321 +11557-4 +13424-3 0 9996
2 07478 062.8068 187.1084 0102525 115.0132 246.1654 15.97292222002613
| Epoch (UTC): | 08 November 1974 02:18:12 |
| Eccentricity: | 0.0102525 |
| inclination: | 62.8068° |
| perigee height: | 213 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 187.1084° |
| argument of perigee: | 115.0132° |
| revolutions per day: | 15.97292222 |
| mean anomaly at epoch: | 246.1654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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