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 33410U 08053C 22148.77524716 .00002749 00000-0 18895-3 0 9999
2 33410 97.8989 155.1047 0125395 257.1528 101.5661 15.00655143741441
| Epoch (UTC): | 28 May 2022 18:36:21 |
| Eccentricity: | 0.0125395 |
| inclination: | 97.8989° |
| perigee height: | 478 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 155.1047° |
| argument of perigee: | 257.1528° |
| revolutions per day: | 15.00655143 |
| mean anomaly at epoch: | 101.5661° |
| orbit number at epoch: | 74144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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