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 48583U 26145.41330140 +.00000000 +00000-0 +42260-4 0 00003
2 48583 53.1615 152.1414 0001454 84.6561 275.4606 15.31694563 06
| Epoch (UTC): | 25 May 2026 09:55:09 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 152.1414° |
| argument of perigee: | 84.6561° |
| revolutions per day: | 15.31694563 |
| mean anomaly at epoch: | 275.4606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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