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 07325U 74040 A 78035.00000005 .00000782 +00000-0 +00000-0 0 9997
2 07325 083.0730 275.8030 8975490 227.8450 259.2170 00.46796613006324
| Epoch (UTC): | 04 February 1978 00:00:00 |
| Eccentricity: | 0.8975490 |
| inclination: | 83.0730° |
| perigee height: | 801 km |
| apogee height: | 126600 km |
| right ascension of ascending node: | 275.8030° |
| argument of perigee: | 227.8450° |
| revolutions per day: | 0.46796613 |
| mean anomaly at epoch: | 259.2170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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