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 27831U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00009
2 27831 6.8360 69.6809 0005921 349.0504 202.3665 1.00271685 00
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0005921 |
| inclination: | 6.8360° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 69.6809° |
| argument of perigee: | 349.0504° |
| revolutions per day: | 1.00271685 |
| mean anomaly at epoch: | 202.3665° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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