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 35951U 26114.11351389 +.00000000 +00000-0 +14637-3 0 00005
2 35951 98.9015 95.0099 0011994 48.6533 311.5669 14.14864488 01
| Epoch (UTC): | 24 April 2026 02:43:27 |
| Eccentricity: | 0.0011994 |
| inclination: | 98.9015° |
| perigee height: | 834 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 95.0099° |
| argument of perigee: | 48.6533° |
| revolutions per day: | 14.14864488 |
| mean anomaly at epoch: | 311.5669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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