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 49080U 26145.32167916 +.00000000 +00000-0 +80558-4 0 00007
2 49080 87.9163 10.4002 0001298 89.8920 270.2360 13.17649789 05
| Epoch (UTC): | 25 May 2026 07:43:13 |
| Eccentricity: | 0.0001298 |
| inclination: | 87.9163° |
| perigee height: | 1193 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4002° |
| argument of perigee: | 89.8920° |
| revolutions per day: | 13.17649789 |
| mean anomaly at epoch: | 270.2360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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