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 48019U 26145.46591543 +.00000000 +00000-0 +78076-4 0 00002
2 48019 53.1597 309.7794 0001391 88.3744 271.7417 15.31705767 02
| Epoch (UTC): | 25 May 2026 11:10:55 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 309.7794° |
| argument of perigee: | 88.3744° |
| revolutions per day: | 15.31705767 |
| mean anomaly at epoch: | 271.7417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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