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 26139.94169553 +.00000000 +00000-0 +13684-3 0 00006
2 48274 41.4672 133.7605 0007514 262.7903 97.2082 15.60684127 00
| Epoch (UTC): | 19 May 2026 22:36:02 |
| Eccentricity: | 0.0007514 |
| inclination: | 41.4672° |
| perigee height: | 381 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 133.7605° |
| argument of perigee: | 262.7903° |
| revolutions per day: | 15.60684127 |
| mean anomaly at epoch: | 97.2082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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