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 38753U 26107.43163873 +.00000000 +00000-0 +65246-3 0 00006
2 38753 10.0351 178.6839 6401248 72.7375 344.5249 3.48233592 06
| Epoch (UTC): | 17 April 2026 10:21:33 |
| Eccentricity: | 0.6401248 |
| inclination: | 10.0351° |
| perigee height: | 239 km |
| apogee height: | 23777 km |
| right ascension of ascending node: | 178.6839° |
| argument of perigee: | 72.7375° |
| revolutions per day: | 3.48233592 |
| mean anomaly at epoch: | 344.5249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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