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 32376U 26070.81083882 +.00000000 +00000-0 +89382-4 0 00001
2 32376 97.8871 255.8162 0001351 83.4458 276.6909 14.82146006 05
| Epoch (UTC): | 11 March 2026 19:27:36 |
| Eccentricity: | 0.0001351 |
| inclination: | 97.8871° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 255.8162° |
| argument of perigee: | 83.4458° |
| revolutions per day: | 14.82146006 |
| mean anomaly at epoch: | 276.6909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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