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 33244U 08036A 23259.85073695 0.00012500 00000-0 45909-3 0 08
2 33244 98.1702 324.8518 0000238 156.8677 203.1322 15.27960576 00
| Epoch (UTC): | 16 September 2023 20:25:03 |
| Eccentricity: | 0.0000238 |
| inclination: | 98.1702° |
| perigee height: | 482 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 324.8518° |
| argument of perigee: | 156.8677° |
| revolutions per day: | 15.27960576 |
| mean anomaly at epoch: | 203.1322° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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