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 33409U 08053B 25340.60844457 .00002645 00000-0 19891-3 0 9995
2 33409 97.8671 352.3177 0019202 334.4031 25.6242 15.03330291933800
| Epoch (UTC): | 06 December 2025 14:36:09 |
| Eccentricity: | 0.0019202 |
| inclination: | 97.8671° |
| perigee height: | 543 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 352.3177° |
| argument of perigee: | 334.4031° |
| revolutions per day: | 15.03330291 |
| mean anomaly at epoch: | 25.6242° |
| orbit number at epoch: | 93380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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