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 48274U 26137.50999963 +.00000000 +00000-0 +12725-3 0 00007
2 48274 41.4666 148.5563 0007424 248.9683 111.0362 15.60632593 07
| Epoch (UTC): | 17 May 2026 12:14:23 |
| Eccentricity: | 0.0007424 |
| inclination: | 41.4666° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 148.5563° |
| argument of perigee: | 248.9683° |
| revolutions per day: | 15.60632593 |
| mean anomaly at epoch: | 111.0362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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