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 27389U 26150.00097027 +.00000000 +00000-0 +00000-0 0 00001
2 27389 12.1347 46.9949 0002409 112.5887 73.0623 0.98984564 01
| Epoch (UTC): | 30 May 2026 00:01:23 |
| Eccentricity: | 0.0002409 |
| inclination: | 12.1347° |
| perigee height: | 36141 km |
| apogee height: | 36162 km |
| right ascension of ascending node: | 46.9949° |
| argument of perigee: | 112.5887° |
| revolutions per day: | 0.98984564 |
| mean anomaly at epoch: | 73.0623° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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