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 22221.16375154 .00000100 00000-0 19076-4 0 9993
2 00059 28.2473 157.5354 0189058 15.8271 344.8086 13.53002785 52326
| Epoch (UTC): | 09 August 2022 03:55:48 |
| Eccentricity: | 0.0189058 |
| inclination: | 28.2473° |
| perigee height: | 920 km |
| apogee height: | 1202 km |
| right ascension of ascending node: | 157.5354° |
| argument of perigee: | 15.8271° |
| revolutions per day: | 13.53002785 |
| mean anomaly at epoch: | 344.8086° |
| orbit number at epoch: | 5232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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