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 33504U 09003A 25196.93884022 .00005137 00000-0 14011-3 0 9992
2 33504 82.4334 160.7457 0009702 289.1828 70.8365 15.37153263909303
| Epoch (UTC): | 15 July 2025 22:31:55 |
| Eccentricity: | 0.0009702 |
| inclination: | 82.4334° |
| perigee height: | 448 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 160.7457° |
| argument of perigee: | 289.1828° |
| revolutions per day: | 15.37153263 |
| mean anomaly at epoch: | 70.8365° |
| orbit number at epoch: | 90930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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