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 38752U 26051.90872740 +.00000000 +00000-0 +76586-3 0 00004
2 38752 9.5684 330.3487 2584439 123.7675 263.5876 10.57756374 05
| Epoch (UTC): | 20 February 2026 21:48:34 |
| Eccentricity: | 0.2584439 |
| inclination: | 9.5684° |
| perigee height: | 122 km |
| apogee height: | 4654 km |
| right ascension of ascending node: | 330.3487° |
| argument of perigee: | 123.7675° |
| revolutions per day: | 10.57756374 |
| mean anomaly at epoch: | 263.5876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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