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 26145.64135545 +.00000000 +00000-0 +25887-3 0 00001
2 32289 97.8171 175.7426 0001926 95.6503 264.4935 14.90681277 05
| Epoch (UTC): | 25 May 2026 15:23:33 |
| Eccentricity: | 0.0001926 |
| inclination: | 97.8171° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 175.7426° |
| argument of perigee: | 95.6503° |
| revolutions per day: | 14.90681277 |
| mean anomaly at epoch: | 264.4935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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