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 27640U 26137.75620860 +.00000000 +00000-0 +47533-4 0 00001
2 27640 98.7134 145.1053 0012957 303.4053 56.5883 14.19935880 07
| Epoch (UTC): | 17 May 2026 18:08:56 |
| Eccentricity: | 0.0012957 |
| inclination: | 98.7134° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 145.1053° |
| argument of perigee: | 303.4053° |
| revolutions per day: | 14.19935880 |
| mean anomaly at epoch: | 56.5883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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