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 26111.00002315 +.00000000 +00000-0 +55527-3 0 00009
2 38358 6.0253 102.9087 0008621 331.8581 102.9813 15.08234307 05
| Epoch (UTC): | 21 April 2026 00:00:02 |
| Eccentricity: | 0.0008621 |
| inclination: | 6.0253° |
| perigee height: | 536 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 102.9087° |
| argument of perigee: | 331.8581° |
| revolutions per day: | 15.08234307 |
| mean anomaly at epoch: | 102.9813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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