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 49396U 26145.05152964 +.00000000 +00000-0 +91505-4 0 00008
2 49396 97.3685 175.4344 0012554 20.8330 339.3409 15.09411383 08
| Epoch (UTC): | 25 May 2026 01:14:12 |
| Eccentricity: | 0.0012554 |
| inclination: | 97.3685° |
| perigee height: | 529 km |
| apogee height: | 547 km |
| right ascension of ascending node: | 175.4344° |
| argument of perigee: | 20.8330° |
| revolutions per day: | 15.09411383 |
| mean anomaly at epoch: | 339.3409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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