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 38358U 26056.91671295 +.00000000 +00000-0 +52258-3 0 00004
2 38358 6.0264 148.0374 0009526 254.8801 266.1133 15.07522625 01
| Epoch (UTC): | 25 February 2026 22:00:03 |
| Eccentricity: | 0.0009526 |
| inclination: | 6.0264° |
| perigee height: | 537 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 148.0374° |
| argument of perigee: | 254.8801° |
| revolutions per day: | 15.07522625 |
| mean anomaly at epoch: | 266.1133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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