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 68548U 26145.59496862 +.00000000 +00000-0 -61619-2 0 00007
2 68548 53.1618 5.0621 0000527 85.0914 275.0149 15.34220646 03
| Epoch (UTC): | 25 May 2026 14:16:45 |
| Eccentricity: | 0.0000527 |
| inclination: | 53.1618° |
| perigee height: | 463 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 5.0621° |
| argument of perigee: | 85.0914° |
| revolutions per day: | 15.34220646 |
| mean anomaly at epoch: | 275.0149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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