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 11112U 26097.10027794 +.00000000 +00000-0 +10535-3 0 00000
2 11112 74.0328 5.3220 0032018 100.4109 260.0657 14.38785500 00
| Epoch (UTC): | 07 April 2026 02:24:24 |
| Eccentricity: | 0.0032018 |
| inclination: | 74.0328° |
| perigee height: | 740 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 5.3220° |
| argument of perigee: | 100.4109° |
| revolutions per day: | 14.38785500 |
| mean anomaly at epoch: | 260.0657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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