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 49734U 26145.37376919 +.00000000 +00000-0 -29405-4 0 00008
2 49734 53.2123 164.8988 0001070 82.7820 277.3294 15.08848810 01
| Epoch (UTC): | 25 May 2026 08:58:13 |
| Eccentricity: | 0.0001070 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.8988° |
| argument of perigee: | 82.7820° |
| revolutions per day: | 15.08848810 |
| mean anomaly at epoch: | 277.3294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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