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 01292U 26100.14056594 +.00000000 +00000-0 +95558-4 0 00006
2 01292 70.0747 97.9452 0017696 32.6005 327.6192 14.01565498 05
| Epoch (UTC): | 10 April 2026 03:22:24 |
| Eccentricity: | 0.0017696 |
| inclination: | 70.0747° |
| perigee height: | 876 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 97.9452° |
| argument of perigee: | 32.6005° |
| revolutions per day: | 14.01565498 |
| mean anomaly at epoch: | 327.6192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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