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 13782U 26150.15313082 +.00000000 +00000-0 +00000-0 0 00001
2 13782 10.3170 320.5993 0010675 333.7253 41.2417 0.99406265 01
| Epoch (UTC): | 30 May 2026 03:40:30 |
| Eccentricity: | 0.0010675 |
| inclination: | 10.3170° |
| perigee height: | 35986 km |
| apogee height: | 36076 km |
| right ascension of ascending node: | 320.5993° |
| argument of perigee: | 333.7253° |
| revolutions per day: | 0.99406265 |
| mean anomaly at epoch: | 41.2417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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