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 25791U 26029.94879817 +.00000000 +00000-0 +14655-3 0 00003
2 25791 24.9834 137.8023 0010429 68.8157 291.3464 14.44391955 05
| Epoch (UTC): | 29 January 2026 22:46:16 |
| Eccentricity: | 0.0010429 |
| inclination: | 24.9834° |
| perigee height: | 737 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 137.8023° |
| argument of perigee: | 68.8157° |
| revolutions per day: | 14.44391955 |
| mean anomaly at epoch: | 291.3464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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