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 26145.61251830 +.00000000 +00000-0 +38740-4 0 00004
2 32376 97.8885 329.5384 0001477 87.8378 272.3004 14.82149006 05
| Epoch (UTC): | 25 May 2026 14:42:01 |
| Eccentricity: | 0.0001477 |
| inclination: | 97.8885° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 329.5384° |
| argument of perigee: | 87.8378° |
| revolutions per day: | 14.82149006 |
| mean anomaly at epoch: | 272.3004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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