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 26074.59144396 +.00000000 +00000-0 +67584-4 0 00008
2 32376 97.8869 259.5421 0001326 84.6896 275.4468 14.82150774 06
| Epoch (UTC): | 15 March 2026 14:11:40 |
| Eccentricity: | 0.0001326 |
| inclination: | 97.8869° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 259.5421° |
| argument of perigee: | 84.6896° |
| revolutions per day: | 14.82150774 |
| mean anomaly at epoch: | 275.4468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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