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 38093U 26032.08711522 +.00000000 +00000-0 +00000-0 0 00005
2 38093 5.1968 47.2057 0054563 356.8915 18.5878 1.00271965 07
| Epoch (UTC): | 01 February 2026 02:05:26 |
| Eccentricity: | 0.0054563 |
| inclination: | 5.1968° |
| perigee height: | 35556 km |
| apogee height: | 36017 km |
| right ascension of ascending node: | 47.2057° |
| argument of perigee: | 356.8915° |
| revolutions per day: | 1.00271965 |
| mean anomaly at epoch: | 18.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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