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 00011U 26140.78684970 +.00000000 +00000-0 +38151-3 0 00008
2 00011 32.8738 188.8587 1445417 260.9643 82.5127 11.90433207 01
| Epoch (UTC): | 20 May 2026 18:53:03 |
| Eccentricity: | 0.1445417 |
| inclination: | 32.8738° |
| perigee height: | 553 km |
| apogee height: | 2895 km |
| right ascension of ascending node: | 188.8587° |
| argument of perigee: | 260.9643° |
| revolutions per day: | 11.90433207 |
| mean anomaly at epoch: | 82.5127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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