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 38780U 26018.80593848 +.00000000 +00000-0 +58814-3 0 00000
2 38780 6.3267 40.4984 6857675 347.0023 1.7736 2.82768798 05
| Epoch (UTC): | 18 January 2026 19:20:33 |
| Eccentricity: | 0.6857675 |
| inclination: | 6.3267° |
| perigee height: | 260 km |
| apogee height: | 29232 km |
| right ascension of ascending node: | 40.4984° |
| argument of perigee: | 347.0023° |
| revolutions per day: | 2.82768798 |
| mean anomaly at epoch: | 1.7736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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