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 61238U 26146.26601064 +.00000000 +00000-0 +22152-3 0 00002
2 61238 97.4476 154.3392 0001895 67.8208 292.3228 15.19153605 04
| Epoch (UTC): | 26 May 2026 06:23:03 |
| Eccentricity: | 0.0001895 |
| inclination: | 97.4476° |
| perigee height: | 507 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 154.3392° |
| argument of perigee: | 67.8208° |
| revolutions per day: | 15.19153605 |
| mean anomaly at epoch: | 292.3228° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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