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 15752U 26044.73183094 +.00000000 +00000-0 +42879-4 0 00008
2 15752 82.9522 132.7559 0023101 334.1679 25.8321 13.73343075 09
| Epoch (UTC): | 13 February 2026 17:33:50 |
| Eccentricity: | 0.0023101 |
| inclination: | 82.9522° |
| perigee height: | 971 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 132.7559° |
| argument of perigee: | 334.1679° |
| revolutions per day: | 13.73343075 |
| mean anomaly at epoch: | 25.8321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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