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 00059U 60013B 21016.55697009 .00000096 00000-0 79014-5 0 9996
2 00059 28.2473 203.5375 0189294 274.8100 83.0855 13.52982364975421
| Epoch (UTC): | 16 January 2021 13:22:02 |
| Eccentricity: | 0.0189294 |
| inclination: | 28.2473° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 203.5375° |
| argument of perigee: | 274.8100° |
| revolutions per day: | 13.52982364 |
| mean anomaly at epoch: | 83.0855° |
| orbit number at epoch: | 97542 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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