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 27943U 26150.46679657 +.00000000 +00000-0 +87714-4 0 00003
2 27943 98.3960 320.2609 0011772 50.9081 309.3168 14.67048150 01
| Epoch (UTC): | 30 May 2026 11:12:11 |
| Eccentricity: | 0.0011772 |
| inclination: | 98.3960° |
| perigee height: | 662 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 320.2609° |
| argument of perigee: | 50.9081° |
| revolutions per day: | 14.67048150 |
| mean anomaly at epoch: | 309.3168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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