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 68139U 26145.73963559 +.00000000 +00000-0 +18308-3 0 00008
2 68139 35.0011 42.3849 0004309 166.9666 193.1151 14.91734324 04
| Epoch (UTC): | 25 May 2026 17:45:04 |
| Eccentricity: | 0.0004309 |
| inclination: | 35.0011° |
| perigee height: | 590 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 42.3849° |
| argument of perigee: | 166.9666° |
| revolutions per day: | 14.91734324 |
| mean anomaly at epoch: | 193.1151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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