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 33393U 08048A 25138.66514447 .00003903 00000-0 29102-3 0 9999
2 33393 9.3440 174.5098 0010059 116.2497 243.8737 14.94214041903761
| Epoch (UTC): | 18 May 2025 15:57:48 |
| Eccentricity: | 0.0010059 |
| inclination: | 9.3440° |
| perigee height: | 578 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 174.5098° |
| argument of perigee: | 116.2497° |
| revolutions per day: | 14.94214041 |
| mean anomaly at epoch: | 243.8737° |
| orbit number at epoch: | 90376 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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