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 is defined by the following mean orbital elements,
1 38078U 12006B 20116.25753030 .27938345 45898-5 14626-3 0 9992
2 38078 69.4046 73.0187 0017419 186.1699 260.1576 16.54569111446689
| Epoch (UTC): | 25 April 2020 06:10:50 |
| Eccentricity: | 0.0017419 |
| inclination: | 69.4046° |
| perigee height: | 116 km |
| apogee height: | 138 km |
| right ascension of ascending node: | 73.0187° |
| argument of perigee: | 186.1699° |
| revolutions per day: | 16.54569111 |
| mean anomaly at epoch: | 260.1576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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