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 00004U 58001 A 70090.03500497 .07718844 +00000-0 +00000-0 0 07809
2 00004 033.1468 334.6171 0024739 311.5310 048.3249 16.27546304584022
| Epoch (UTC): | 31 March 1970 00:50:24 |
| Eccentricity: | 0.0024739 |
| inclination: | 33.1468° |
| perigee height: | 183 km |
| apogee height: | 215 km |
| right ascension of ascending node: | 334.6171° |
| argument of perigee: | 311.5310° |
| revolutions per day: | 16.27546304 |
| mean anomaly at epoch: | 48.3249° |
| orbit number at epoch: | 58402 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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