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 is defined by the following mean orbital elements,
1 38012U 26032.51015295 +.00000000 +00000-0 +10509-3 0 00006
2 38012 98.1754 109.4779 0001195 104.6923 8.9792 14.58566861 03
| Epoch (UTC): | 01 February 2026 12:14:37 |
| Eccentricity: | 0.0001195 |
| inclination: | 98.1754° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 109.4779° |
| argument of perigee: | 104.6923° |
| revolutions per day: | 14.58566861 |
| mean anomaly at epoch: | 8.9792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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