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 26109.29187434 +.00000000 +00000-0 +43963-4 0 00009
2 32376 97.8884 293.7428 0001380 91.6987 268.4384 14.82153758 03
| Epoch (UTC): | 19 April 2026 07:00:17 |
| Eccentricity: | 0.0001380 |
| inclination: | 97.8884° |
| perigee height: | 622 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 293.7428° |
| argument of perigee: | 91.6987° |
| revolutions per day: | 14.82153758 |
| mean anomaly at epoch: | 268.4384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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