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 38745U 26152.12291081 +.00000000 +00000-0 +64101-3 0 00005
2 38745 49.8228 116.1370 1574170 128.5736 246.7006 12.42244990 00
| Epoch (UTC): | 01 June 2026 02:56:59 |
| Eccentricity: | 0.1574170 |
| inclination: | 49.8228° |
| perigee height: | 257 km |
| apogee height: | 2737 km |
| right ascension of ascending node: | 116.1370° |
| argument of perigee: | 128.5736° |
| revolutions per day: | 12.42244990 |
| mean anomaly at epoch: | 246.7006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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