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 26140.53427530 +.00000000 +00000-0 +00000-0 0 00008
2 38093 5.4207 47.1729 0059300 359.7353 283.7017 1.00271902 05
| Epoch (UTC): | 20 May 2026 12:49:21 |
| Eccentricity: | 0.0059300 |
| inclination: | 5.4207° |
| perigee height: | 35537 km |
| apogee height: | 36037 km |
| right ascension of ascending node: | 47.1729° |
| argument of perigee: | 359.7353° |
| revolutions per day: | 1.00271902 |
| mean anomaly at epoch: | 283.7017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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