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 68347U 26145.58703965 +.00000000 +00000-0 +70309-3 0 00004
2 68347 53.1576 350.7446 0001082 99.9391 260.1732 15.30205916 00
| Epoch (UTC): | 25 May 2026 14:05:20 |
| Eccentricity: | 0.0001082 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 350.7446° |
| argument of perigee: | 99.9391° |
| revolutions per day: | 15.30205916 |
| mean anomaly at epoch: | 260.1732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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