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 25109.49568650 .00005379 00000-0 41055-3 0 9997
2 33409 97.8752 117.5246 0020453 31.1138 329.1293 15.02267635899097
| Epoch (UTC): | 19 April 2025 11:53:47 |
| Eccentricity: | 0.0020453 |
| inclination: | 97.8752° |
| perigee height: | 546 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 117.5246° |
| argument of perigee: | 31.1138° |
| revolutions per day: | 15.02267635 |
| mean anomaly at epoch: | 329.1293° |
| orbit number at epoch: | 89909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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