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 25077U 26088.14714433 +.00000000 +00000-0 +12233-3 0 00009
2 25077 86.3930 119.8854 0001460 95.9544 264.1820 14.36636578 07
| Epoch (UTC): | 29 March 2026 03:31:53 |
| Eccentricity: | 0.0001460 |
| inclination: | 86.3930° |
| perigee height: | 769 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 119.8854° |
| argument of perigee: | 95.9544° |
| revolutions per day: | 14.36636578 |
| mean anomaly at epoch: | 264.1820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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