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 48589U 26145.13266251 +.00000000 +00000-0 +67778-5 0 00001
2 48589 53.1586 131.2464 0001182 99.3074 260.8061 15.31698678 06
| Epoch (UTC): | 25 May 2026 03:11:02 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1586° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 131.2464° |
| argument of perigee: | 99.3074° |
| revolutions per day: | 15.31698678 |
| mean anomaly at epoch: | 260.8061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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