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 68328U 26145.54599630 +.00000000 +00000-0 +59042-3 0 00002
2 68328 53.1581 351.2102 0001373 80.5630 279.5526 15.30209545 02
| Epoch (UTC): | 25 May 2026 13:06:14 |
| Eccentricity: | 0.0001373 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.2102° |
| argument of perigee: | 80.5630° |
| revolutions per day: | 15.30209545 |
| mean anomaly at epoch: | 279.5526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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