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 32768U 26145.49953831 +.00000000 +00000-0 +00000-0 0 00009
2 32768 1.1852 82.6530 0002775 337.4244 297.8418 1.00274141 06
| Epoch (UTC): | 25 May 2026 11:59:20 |
| Eccentricity: | 0.0002775 |
| inclination: | 1.1852° |
| perigee height: | 35774 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 82.6530° |
| argument of perigee: | 337.4244° |
| revolutions per day: | 1.00274141 |
| mean anomaly at epoch: | 297.8418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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