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 48289U 26145.53490830 +.00000000 +00000-0 +27427-4 0 00000
2 48289 53.1602 78.2741 0001401 75.0878 285.0278 15.31695986 05
| Epoch (UTC): | 25 May 2026 12:50:16 |
| Eccentricity: | 0.0001401 |
| inclination: | 53.1602° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.2741° |
| argument of perigee: | 75.0878° |
| revolutions per day: | 15.31695986 |
| mean anomaly at epoch: | 285.0278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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