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 26064.32984588 +.00000000 +00000-0 +10249-3 0 00008
2 32376 97.8861 249.4290 0001309 83.5304 276.6058 14.82159256 05
| Epoch (UTC): | 05 March 2026 07:54:58 |
| Eccentricity: | 0.0001309 |
| inclination: | 97.8861° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 249.4290° |
| argument of perigee: | 83.5304° |
| revolutions per day: | 14.82159256 |
| mean anomaly at epoch: | 276.6058° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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