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 12139U 81003B 25198.38740366 .00010203 00000-0 30239-3 0 9996
2 12139 82.9338 145.9742 0297819 271.0008 85.7113 15.00836116279258
| Epoch (UTC): | 17 July 2025 09:17:51 |
| Eccentricity: | 0.0297819 |
| inclination: | 82.9338° |
| perigee height: | 357 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 145.9742° |
| argument of perigee: | 271.0008° |
| revolutions per day: | 15.00836116 |
| mean anomaly at epoch: | 85.7113° |
| orbit number at epoch: | 27925 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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