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 49757U 26145.45292648 +.00000000 +00000-0 -70251-4 0 00003
2 49757 53.2101 154.5288 0001078 77.7939 282.3173 15.08845439 00
| Epoch (UTC): | 25 May 2026 10:52:12 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.2101° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 154.5288° |
| argument of perigee: | 77.7939° |
| revolutions per day: | 15.08845439 |
| mean anomaly at epoch: | 282.3173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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