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 13771U 83003B 25188.48013493 .00005392 00000-0 18560-3 0 9991
2 13771 81.1583 194.4410 0030431 276.8479 82.9295 15.29408726318858
| Epoch (UTC): | 07 July 2025 11:31:23 |
| Eccentricity: | 0.0030431 |
| inclination: | 81.1583° |
| perigee height: | 457 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 194.4410° |
| argument of perigee: | 276.8479° |
| revolutions per day: | 15.29408726 |
| mean anomaly at epoch: | 82.9295° |
| orbit number at epoch: | 31885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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