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 32289U 26065.62063505 +.00000000 +00000-0 +40568-3 0 00009
2 32289 97.8270 96.4834 0001735 84.4472 275.6943 14.90344416 00
| Epoch (UTC): | 06 March 2026 14:53:42 |
| Eccentricity: | 0.0001735 |
| inclination: | 97.8270° |
| perigee height: | 596 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 96.4834° |
| argument of perigee: | 84.4472° |
| revolutions per day: | 14.90344416 |
| mean anomaly at epoch: | 275.6943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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