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 06153U 72065A 21023.60319713 .00000018 00000-0 82245-5 0 9998
2 06153 35.0064 135.6150 0006916 358.2225 117.3956 14.57966428572834
| Epoch (UTC): | 23 January 2021 14:28:36 |
| Eccentricity: | 0.0006916 |
| inclination: | 35.0064° |
| perigee height: | 695 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 135.6150° |
| argument of perigee: | 358.2225° |
| revolutions per day: | 14.57966428 |
| mean anomaly at epoch: | 117.3956° |
| orbit number at epoch: | 57283 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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