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 26032.53234882 +.00000000 +00000-0 +10054-3 0 00005
2 32376 97.8837 218.0969 0001534 81.1431 278.9956 14.82113398 07
| Epoch (UTC): | 01 February 2026 12:46:34 |
| Eccentricity: | 0.0001534 |
| inclination: | 97.8837° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 218.0969° |
| argument of perigee: | 81.1431° |
| revolutions per day: | 14.82113398 |
| mean anomaly at epoch: | 278.9956° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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