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 32785U 26106.25438213 +.00000000 +00000-0 +16008-3 0 00009
2 32785 97.8246 86.4279 0007395 232.2641 127.7917 15.08862338 01
| Epoch (UTC): | 16 April 2026 06:06:18 |
| Eccentricity: | 0.0007395 |
| inclination: | 97.8246° |
| perigee height: | 535 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 86.4279° |
| argument of perigee: | 232.2641° |
| revolutions per day: | 15.08862338 |
| mean anomaly at epoch: | 127.7917° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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