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 32959U 26160.09490499 +.00000000 +00000-0 +45968-4 0 00006
2 32959 98.8544 231.3640 0067808 295.4474 125.5649 14.43029831 08
| Epoch (UTC): | 09 June 2026 02:16:39 |
| Eccentricity: | 0.0067808 |
| inclination: | 98.8544° |
| perigee height: | 700 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 231.3640° |
| argument of perigee: | 295.4474° |
| revolutions per day: | 14.43029831 |
| mean anomaly at epoch: | 125.5649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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