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 26022.27078287 +.00000000 +00000-0 +20745-3 0 00008
2 32376 97.8820 207.9872 0001282 86.1225 274.0135 14.82172773 03
| Epoch (UTC): | 22 January 2026 06:29:55 |
| Eccentricity: | 0.0001282 |
| inclination: | 97.8820° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 207.9872° |
| argument of perigee: | 86.1225° |
| revolutions per day: | 14.82172773 |
| mean anomaly at epoch: | 274.0135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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