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 27534U 26104.16235985 +.00000000 +00000-0 +35622-4 0 00008
2 27534 82.9395 18.0783 0036744 148.8109 15.9395 13.72956670 09
| Epoch (UTC): | 14 April 2026 03:53:47 |
| Eccentricity: | 0.0036744 |
| inclination: | 82.9395° |
| perigee height: | 962 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 18.0783° |
| argument of perigee: | 148.8109° |
| revolutions per day: | 13.72956670 |
| mean anomaly at epoch: | 15.9395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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