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 48554U 26145.35170473 +.00000000 +00000-0 +48325-4 0 00003
2 48554 53.1590 130.1450 0001444 94.9757 265.1409 15.31703188 03
| Epoch (UTC): | 25 May 2026 08:26:27 |
| Eccentricity: | 0.0001444 |
| inclination: | 53.1590° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 130.1450° |
| argument of perigee: | 94.9757° |
| revolutions per day: | 15.31703188 |
| mean anomaly at epoch: | 265.1409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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