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 49079U 26145.57634039 +.00000000 +00000-0 -52833-3 0 00002
2 49079 87.9157 10.3784 0001464 90.5408 269.5891 13.17648861 07
| Epoch (UTC): | 25 May 2026 13:49:55 |
| Eccentricity: | 0.0001464 |
| inclination: | 87.9157° |
| perigee height: | 1193 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3784° |
| argument of perigee: | 90.5408° |
| revolutions per day: | 13.17648861 |
| mean anomaly at epoch: | 269.5891° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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