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 1328U 65032A 19053.90163758 -.00000086 +00000-0 -64663-6 0 9994
2 1328 041.1839 284.4743 0255001 090.8799 272.1178 13.38590425630769
| Epoch (UTC): | 22 February 2019 21:38:21 |
| Eccentricity: | 0.0255001 |
| inclination: | 41.1839° |
| perigee height: | 923 km |
| apogee height: | 1305 km |
| right ascension of ascending node: | 284.4743° |
| argument of perigee: | 90.8799° |
| revolutions per day: | 13.38590425 |
| mean anomaly at epoch: | 272.1178° |
| orbit number at epoch: | 63076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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