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 20465U 90010A 23151.93862184 .00002656 00000-0 20827-3 0 9991
2 20465 82.4864 314.4376 0015187 157.3888 202.8009 15.00511038810960
| Epoch (UTC): | 31 May 2023 22:31:36 |
| Eccentricity: | 0.0015187 |
| inclination: | 82.4864° |
| perigee height: | 555 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 314.4376° |
| argument of perigee: | 157.3888° |
| revolutions per day: | 15.00511038 |
| mean anomaly at epoch: | 202.8009° |
| orbit number at epoch: | 81096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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