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 26042.18187605 +.00000000 +00000-0 +56926-4 0 00005
2 15752 82.9524 134.6368 0023267 341.4322 18.5982 13.73342924 03
| Epoch (UTC): | 11 February 2026 04:21:54 |
| Eccentricity: | 0.0023267 |
| inclination: | 82.9524° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 134.6368° |
| argument of perigee: | 341.4322° |
| revolutions per day: | 13.73342924 |
| mean anomaly at epoch: | 18.5982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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