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 33323U 08041D 23033.55636481 .00006526 00000-0 62020-3 0 9998
2 33323 97.5838 20.9849 0020241 323.8464 150.9135 14.93648101780070
| Epoch (UTC): | 02 February 2023 13:21:09 |
| Eccentricity: | 0.0020241 |
| inclination: | 97.5838° |
| perigee height: | 572 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 20.9849° |
| argument of perigee: | 323.8464° |
| revolutions per day: | 14.93648101 |
| mean anomaly at epoch: | 150.9135° |
| orbit number at epoch: | 78007 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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