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 38466U 12033A 19028.13742259 0.00000000 00000-0 00000-0 0 02
2 38466 1.5655 152.6082 0003453 140.5774 219.4640 1.00270000 04
| Epoch (UTC): | 28 January 2019 03:17:53 |
| Eccentricity: | 0.0003453 |
| inclination: | 1.5655° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 152.6082° |
| argument of perigee: | 140.5774° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 219.4640° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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