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 63138U 26145.30885329 +.00000000 +00000-0 +12890-2 0 00002
2 63138 43.0024 148.7631 0001278 239.9958 120.0783 15.70979220 02
| Epoch (UTC): | 25 May 2026 07:24:44 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0024° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 148.7631° |
| argument of perigee: | 239.9958° |
| revolutions per day: | 15.70979220 |
| mean anomaly at epoch: | 120.0783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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