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 27509U 26150.44494367 +.00000000 +00000-0 +00000-0 0 00001
2 27509 11.2221 41.4038 0014116 70.2908 159.6915 0.97903997 02
| Epoch (UTC): | 30 May 2026 10:40:43 |
| Eccentricity: | 0.0014116 |
| inclination: | 11.2221° |
| perigee height: | 36403 km |
| apogee height: | 36524 km |
| right ascension of ascending node: | 41.4038° |
| argument of perigee: | 70.2908° |
| revolutions per day: | 0.97903997 |
| mean anomaly at epoch: | 159.6915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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