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 22219.31907184 .00000106 00000-0 26904-4 0 9995
2 00059 28.2473 167.0116 0189047 0.3357 359.7295 13.53002719 52076
| Epoch (UTC): | 07 August 2022 07:39:27 |
| Eccentricity: | 0.0189047 |
| inclination: | 28.2473° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 167.0116° |
| argument of perigee: | 0.3357° |
| revolutions per day: | 13.53002719 |
| mean anomaly at epoch: | 359.7295° |
| orbit number at epoch: | 5207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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