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 26065.25501414 +.00000000 +00000-0 +14430-3 0 00003
2 25791 24.9840 280.4489 0010307 81.2820 278.8855 14.44420508 05
| Epoch (UTC): | 06 March 2026 06:07:13 |
| Eccentricity: | 0.0010307 |
| inclination: | 24.9840° |
| perigee height: | 737 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 280.4489° |
| argument of perigee: | 81.2820° |
| revolutions per day: | 14.44420508 |
| mean anomaly at epoch: | 278.8855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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