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 25347.33877844 .00019746 00000-0 47286-3 0 9999
2 33504 82.4315 5.4854 0013267 106.4813 253.7892 15.41209881932434
| Epoch (UTC): | 13 December 2025 08:07:50 |
| Eccentricity: | 0.0013267 |
| inclination: | 82.4315° |
| perigee height: | 433 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 5.4854° |
| argument of perigee: | 106.4813° |
| revolutions per day: | 15.41209881 |
| mean anomaly at epoch: | 253.7892° |
| orbit number at epoch: | 93243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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