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 32955U 26145.58468185 +.00000000 +00000-0 +13531-2 0 00005
2 32955 82.5042 6.8965 0021454 356.5514 3.5415 12.43369132 08
| Epoch (UTC): | 25 May 2026 14:01:56 |
| Eccentricity: | 0.0021454 |
| inclination: | 82.5042° |
| perigee height: | 1475 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 6.8965° |
| argument of perigee: | 356.5514° |
| revolutions per day: | 12.43369132 |
| mean anomaly at epoch: | 3.5415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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