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 44752U 26145.27445742 +.00000000 +00000-0 +34071-3 0 00006
2 44752 53.0679 147.7737 0003633 84.8492 275.2923 15.34131402 04
| Epoch (UTC): | 25 May 2026 06:35:13 |
| Eccentricity: | 0.0003633 |
| inclination: | 53.0679° |
| perigee height: | 461 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 147.7737° |
| argument of perigee: | 84.8492° |
| revolutions per day: | 15.34131402 |
| mean anomaly at epoch: | 275.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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