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 48687U 26145.48117382 +.00000000 +00000-0 +10610-3 0 00009
2 48687 53.1585 67.8210 0000982 85.6780 274.4334 15.31722420 03
| Epoch (UTC): | 25 May 2026 11:32:53 |
| Eccentricity: | 0.0000982 |
| inclination: | 53.1585° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 67.8210° |
| argument of perigee: | 85.6780° |
| revolutions per day: | 15.31722420 |
| mean anomaly at epoch: | 274.4334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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