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 48431U 26145.29297231 +.00000000 +00000-0 +38267-4 0 00006
2 48431 53.1602 156.5151 0001341 92.0541 268.0614 15.31701215 06
| Epoch (UTC): | 25 May 2026 07:01:52 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 156.5151° |
| argument of perigee: | 92.0541° |
| revolutions per day: | 15.31701215 |
| mean anomaly at epoch: | 268.0614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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