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 26154.60669470 +.00000000 +00000-0 +00000-0 0 00000
2 27831 6.8560 69.5733 0005945 359.0038 197.6191 1.00271091 07
| Epoch (UTC): | 03 June 2026 14:33:38 |
| Eccentricity: | 0.0005945 |
| inclination: | 6.8560° |
| perigee height: | 35762 km |
| apogee height: | 35812 km |
| right ascension of ascending node: | 69.5733° |
| argument of perigee: | 359.0038° |
| revolutions per day: | 1.00271091 |
| mean anomaly at epoch: | 197.6191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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