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 26040.79761490 +.00000000 +00000-0 +62322-4 0 00007
2 15752 82.9525 135.6579 0023369 345.3367 14.7108 13.73342764 04
| Epoch (UTC): | 09 February 2026 19:08:33 |
| Eccentricity: | 0.0023369 |
| inclination: | 82.9525° |
| perigee height: | 970 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 135.6579° |
| argument of perigee: | 345.3367° |
| revolutions per day: | 13.73342764 |
| mean anomaly at epoch: | 14.7108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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