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 48581U 26145.28137449 +.00000000 +00000-0 +42515-4 0 00006
2 48581 53.1597 107.6191 0001182 73.4210 286.6921 15.31700474 08
| Epoch (UTC): | 25 May 2026 06:45:10 |
| Eccentricity: | 0.0001182 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 107.6191° |
| argument of perigee: | 73.4210° |
| revolutions per day: | 15.31700474 |
| mean anomaly at epoch: | 286.6921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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