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 38109U 12014A 26004.23950474 0.00000080 00000-0 14322-3 0 01
2 38109 122.9990 327.0931 0002693 246.5785 113.4215 13.41451777 04
| Epoch (UTC): | 04 January 2026 05:44:53 |
| Eccentricity: | 0.0002693 |
| inclination: | 122.9990° |
| perigee height: | 1102 km |
| apogee height: | 1106 km |
| right ascension of ascending node: | 327.0931° |
| argument of perigee: | 246.5785° |
| revolutions per day: | 13.41451777 |
| mean anomaly at epoch: | 113.4215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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