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 34111U 26145.50499836 +.00000000 +00000-0 +00000-0 0 00005
2 34111 0.0159 337.1470 0002542 71.7135 338.4816 1.00270381 04
| Epoch (UTC): | 25 May 2026 12:07:11 |
| Eccentricity: | 0.0002542 |
| inclination: | 0.0159° |
| perigee height: | 35776 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 337.1470° |
| argument of perigee: | 71.7135° |
| revolutions per day: | 1.00270381 |
| mean anomaly at epoch: | 338.4816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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