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 26069.51471476 +.00000000 +00000-0 +52418-3 0 00008
2 32289 97.8278 100.3426 0001891 81.0926 279.0506 14.90375217 06
| Epoch (UTC): | 10 March 2026 12:21:11 |
| Eccentricity: | 0.0001891 |
| inclination: | 97.8278° |
| perigee height: | 595 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 100.3426° |
| argument of perigee: | 81.0926° |
| revolutions per day: | 14.90375217 |
| mean anomaly at epoch: | 279.0506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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