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 49724U 26145.49155501 +.00000000 +00000-0 +29525-4 0 00004
2 49724 53.2130 164.5660 0001044 73.2267 286.8840 15.08836269 00
| Epoch (UTC): | 25 May 2026 11:47:50 |
| Eccentricity: | 0.0001044 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.5660° |
| argument of perigee: | 73.2267° |
| revolutions per day: | 15.08836269 |
| mean anomaly at epoch: | 286.8840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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