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 48586U 26145.32009473 +.00000000 +00000-0 +27954-4 0 00001
2 48586 53.1614 152.5137 0001181 98.4813 261.6322 15.31697313 02
| Epoch (UTC): | 25 May 2026 07:40:56 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1614° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 152.5137° |
| argument of perigee: | 98.4813° |
| revolutions per day: | 15.31697313 |
| mean anomaly at epoch: | 261.6322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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