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 38341U 12025E 25137.07338126 .00001659 00000-0 16345-3 0 9990
2 38341 98.4366 76.8468 0045965 200.2121 159.7278 14.92870843704010
| Epoch (UTC): | 17 May 2025 01:45:40 |
| Eccentricity: | 0.0045965 |
| inclination: | 98.4366° |
| perigee height: | 557 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 76.8468° |
| argument of perigee: | 200.2121° |
| revolutions per day: | 14.92870843 |
| mean anomaly at epoch: | 159.7278° |
| orbit number at epoch: | 70401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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