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 39152U 26039.18964015 +.00000000 +00000-0 +47691-3 0 00007
2 39152 97.7944 130.6501 0012723 165.3980 194.7611 14.95452325 04
| Epoch (UTC): | 08 February 2026 04:33:04 |
| Eccentricity: | 0.0012723 |
| inclination: | 97.7944° |
| perigee height: | 572 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 130.6501° |
| argument of perigee: | 165.3980° |
| revolutions per day: | 14.95452325 |
| mean anomaly at epoch: | 194.7611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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