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 48131U 26145.43312931 +.00000000 +00000-0 +43876-5 0 00007
2 48131 53.1612 155.9104 0001084 75.5634 284.5488 15.31704089 02
| Epoch (UTC): | 25 May 2026 10:23:42 |
| Eccentricity: | 0.0001084 |
| inclination: | 53.1612° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 155.9104° |
| argument of perigee: | 75.5634° |
| revolutions per day: | 15.31704089 |
| mean anomaly at epoch: | 284.5488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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