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 38782U 26088.16583198 +.00000000 +00000-0 +21051-3 0 00008
2 38782 97.6097 68.6324 0018781 134.5094 225.7657 14.79851953 04
| Epoch (UTC): | 29 March 2026 03:58:47 |
| Eccentricity: | 0.0018781 |
| inclination: | 97.6097° |
| perigee height: | 617 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 68.6324° |
| argument of perigee: | 134.5094° |
| revolutions per day: | 14.79851953 |
| mean anomaly at epoch: | 225.7657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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