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 48455U 26145.53245941 +.00000000 +00000-0 +39858-4 0 00007
2 48455 53.1592 180.9807 0001273 81.4321 278.6824 15.31704800 04
| Epoch (UTC): | 25 May 2026 12:46:44 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 180.9807° |
| argument of perigee: | 81.4321° |
| revolutions per day: | 15.31704800 |
| mean anomaly at epoch: | 278.6824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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