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 21949U 92023A 19031.19677565 0.00000000 00000-0 00000-0 0 04
2 21949 85.0097 186.8742 0004000 59.0910 300.9089 14.31424421 05
| Epoch (UTC): | 31 January 2019 04:43:21 |
| Eccentricity: | 0.0004000 |
| inclination: | 85.0097° |
| perigee height: | 784 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 186.8742° |
| argument of perigee: | 59.0910° |
| revolutions per day: | 14.31424421 |
| mean anomaly at epoch: | 300.9089° |
| 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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