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 67548U 26145.26627639 +.00000000 +00000-0 +77314-3 0 00007
2 67548 97.2845 32.3829 0001122 94.6316 265.5055 15.33462287 08
| Epoch (UTC): | 25 May 2026 06:23:26 |
| Eccentricity: | 0.0001122 |
| inclination: | 97.2845° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 32.3829° |
| argument of perigee: | 94.6316° |
| revolutions per day: | 15.33462287 |
| mean anomaly at epoch: | 265.5055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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