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 38756U 26039.20054447 +.00000000 +00000-0 +30945-3 0 00002
2 38756 98.2366 317.2167 0012104 107.0127 253.2413 14.82182360 03
| Epoch (UTC): | 08 February 2026 04:48:47 |
| Eccentricity: | 0.0012104 |
| inclination: | 98.2366° |
| perigee height: | 614 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 317.2167° |
| argument of perigee: | 107.0127° |
| revolutions per day: | 14.82182360 |
| mean anomaly at epoch: | 253.2413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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