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 26483U 26150.26603953 +.00000000 +00000-0 +00000-0 0 00004
2 26483 67.0946 43.2926 0207309 247.4027 293.7958 1.64982212 08
| Epoch (UTC): | 30 May 2026 06:23:05 |
| Eccentricity: | 0.0207309 |
| inclination: | 67.0946° |
| perigee height: | 23248 km |
| apogee height: | 24503 km |
| right ascension of ascending node: | 43.2926° |
| argument of perigee: | 247.4027° |
| revolutions per day: | 1.64982212 |
| mean anomaly at epoch: | 293.7958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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