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 data is extracted from the following two-line orbital elements,
1 03955U 69046 E 84131.00025463 .00000569 +00000-0 +00000-0 0 00872
2 03955 061.0496 050.4191 3336010 080.9349 045.4097 00.21490366011775
| Epoch (UTC): | 10 May 1984 00:00:22 |
| Eccentricity: | 0.3336010 |
| inclination: | 61.0496° |
| perigee height: | 72079 km |
| apogee height: | 150632 km |
| right ascension of ascending node: | 50.4191° |
| argument of perigee: | 80.9349° |
| revolutions per day: | 0.21490366 |
| mean anomaly at epoch: | 45.4097° |
| orbit number at epoch: | 1177 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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