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 61548U 26145.58335647 +.00000000 +00000-0 +14295-2 0 00009
2 61548 53.1604 16.9168 0001540 95.9652 53.4267 15.33522867 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001540 |
| inclination: | 53.1604° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 16.9168° |
| argument of perigee: | 95.9652° |
| revolutions per day: | 15.33522867 |
| mean anomaly at epoch: | 53.4267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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