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 68268U 26145.51839024 +.00000000 +00000-0 +11190-2 0 00007
2 68268 53.1584 320.9653 0001016 94.5744 265.5375 15.34423143 00
| Epoch (UTC): | 25 May 2026 12:26:28 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1584° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 320.9653° |
| argument of perigee: | 94.5744° |
| revolutions per day: | 15.34423143 |
| mean anomaly at epoch: | 265.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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