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 39446U 26073.14359576 +.00000000 +00000-0 +52912-3 0 00009
2 39446 97.8592 28.6921 0047984 276.7987 82.7775 14.96235016 07
| Epoch (UTC): | 14 March 2026 03:26:46 |
| Eccentricity: | 0.0047984 |
| inclination: | 97.8592° |
| perigee height: | 545 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 28.6921° |
| argument of perigee: | 276.7987° |
| revolutions per day: | 14.96235016 |
| mean anomaly at epoch: | 82.7775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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