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 26041.40423494 +.00000000 +00000-0 +97099-3 0 00000
2 38745 49.8284 111.7397 1609947 191.0661 165.0317 12.34246335 09
| Epoch (UTC): | 10 February 2026 09:42:05 |
| Eccentricity: | 0.1609947 |
| inclination: | 49.8284° |
| perigee height: | 258 km |
| apogee height: | 2804 km |
| right ascension of ascending node: | 111.7397° |
| argument of perigee: | 191.0661° |
| revolutions per day: | 12.34246335 |
| mean anomaly at epoch: | 165.0317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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