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 49733U 26145.35443735 +.00000000 +00000-0 +10450-3 0 00004
2 49733 53.2157 174.9588 0001588 82.5804 277.5368 15.08848545 08
| Epoch (UTC): | 25 May 2026 08:30:23 |
| Eccentricity: | 0.0001588 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.9588° |
| argument of perigee: | 82.5804° |
| revolutions per day: | 15.08848545 |
| mean anomaly at epoch: | 277.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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