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 38771U 12049A 25341.30236777 .00000284 00000-0 15005-3 0 9990
2 38771 98.6806 31.3531 0002684 156.1748 203.9555 14.21405376686005
| Epoch (UTC): | 07 December 2025 07:15:24 |
| Eccentricity: | 0.0002684 |
| inclination: | 98.6806° |
| perigee height: | 818 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 31.3531° |
| argument of perigee: | 156.1748° |
| revolutions per day: | 14.21405376 |
| mean anomaly at epoch: | 203.9555° |
| orbit number at epoch: | 68600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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