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 20624U 90046A 23156.56138056 -.00000221 00000-0 -90688-4 0 9996
2 20624 71.0406 332.2821 0016972 298.7874 61.1543 14.14467932705053
| Epoch (UTC): | 05 June 2023 13:28:23 |
| Eccentricity: | 0.0016972 |
| inclination: | 71.0406° |
| perigee height: | 832 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 332.2821° |
| argument of perigee: | 298.7874° |
| revolutions per day: | 14.14467932 |
| mean anomaly at epoch: | 61.1543° |
| orbit number at epoch: | 70505 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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