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 49286U 26145.66760735 +.00000000 +00000-0 -11526-4 0 00000
2 49286 87.9176 278.9304 0001972 104.3503 255.7849 13.20773571 03
| Epoch (UTC): | 25 May 2026 16:01:21 |
| Eccentricity: | 0.0001972 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9304° |
| argument of perigee: | 104.3503° |
| revolutions per day: | 13.20773571 |
| mean anomaly at epoch: | 255.7849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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