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 03954U 69046D 84183.00025463 -.00000344 +00000-0 +10000-3 0 00043
2 03954 061.5932 051.6530 2911378 079.9637 110.9535 00.29113780011873
| Epoch (UTC): | 01 July 1984 00:00:22 |
| Eccentricity: | 0.2911378 |
| inclination: | 61.5932° |
| perigee height: | 61787 km |
| apogee height: | 117780 km |
| right ascension of ascending node: | 51.6530° |
| argument of perigee: | 79.9637° |
| revolutions per day: | 0.29113780 |
| mean anomaly at epoch: | 110.9535° |
| orbit number at epoch: | 1187 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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