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 38089U 26157.30458382 +.00000000 +00000-0 +10483-2 0 00003
2 38089 49.6106 12.2220 4941359 121.4085 296.2873 5.70433008 08
| Epoch (UTC): | 06 June 2026 07:18:36 |
| Eccentricity: | 0.4941359 |
| inclination: | 49.6106° |
| perigee height: | 315 km |
| apogee height: | 13391 km |
| right ascension of ascending node: | 12.2220° |
| argument of perigee: | 121.4085° |
| revolutions per day: | 5.70433008 |
| mean anomaly at epoch: | 296.2873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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