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 26145.58258420 +.00000000 +00000-0 +14870-3 0 00001
2 35951 98.9030 126.4026 0010327 320.6781 39.3641 14.14882733 02
| Epoch (UTC): | 25 May 2026 13:58:55 |
| Eccentricity: | 0.0010327 |
| inclination: | 98.9030° |
| perigee height: | 835 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 126.4026° |
| argument of perigee: | 320.6781° |
| revolutions per day: | 14.14882733 |
| mean anomaly at epoch: | 39.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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