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 04366U 70027A 84245.00025463 -.00000798 +00000-0 +10000-3 0 00033
2 04366 031.1700 056.1602 0848739 082.8200 116.9496 00.21521453004892
| Epoch (UTC): | 01 September 1984 00:00:22 |
| Eccentricity: | 0.0848739 |
| inclination: | 31.1700° |
| perigee height: | 101260 km |
| apogee height: | 121226 km |
| right ascension of ascending node: | 56.1602° |
| argument of perigee: | 82.8200° |
| revolutions per day: | 0.21521453 |
| mean anomaly at epoch: | 116.9496° |
| orbit number at epoch: | 489 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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