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 26114.15263170 +.00000000 +00000-0 +45516-4 0 00008
2 32376 97.8885 298.5335 0001393 92.3831 267.7542 14.82157017 04
| Epoch (UTC): | 24 April 2026 03:39:47 |
| Eccentricity: | 0.0001393 |
| inclination: | 97.8885° |
| perigee height: | 622 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 298.5335° |
| argument of perigee: | 92.3831° |
| revolutions per day: | 14.82157017 |
| mean anomaly at epoch: | 267.7542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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