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 49743U 26145.45199558 +.00000000 +00000-0 -20101-4 0 00003
2 49743 53.2135 164.4532 0001086 95.2747 264.8369 15.08846158 06
| Epoch (UTC): | 25 May 2026 10:50:52 |
| Eccentricity: | 0.0001086 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.4532° |
| argument of perigee: | 95.2747° |
| revolutions per day: | 15.08846158 |
| mean anomaly at epoch: | 264.8369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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