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 44753U 26145.32222051 +.00000000 +00000-0 +43935-3 0 00008
2 44753 53.0443 155.3901 0007269 12.6827 347.4369 15.65768233 00
| Epoch (UTC): | 25 May 2026 07:43:59 |
| Eccentricity: | 0.0007269 |
| inclination: | 53.0443° |
| perigee height: | 366 km |
| apogee height: | 376 km |
| right ascension of ascending node: | 155.3901° |
| argument of perigee: | 12.6827° |
| revolutions per day: | 15.65768233 |
| mean anomaly at epoch: | 347.4369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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