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 42183U 26098.74549138 +.00000000 +00000-0 +90687-3 0 00000
2 42183 82.9362 262.0374 0048098 274.7722 100.9051 13.87452557 07
| Epoch (UTC): | 08 April 2026 17:53:30 |
| Eccentricity: | 0.0048098 |
| inclination: | 82.9362° |
| perigee height: | 902 km |
| apogee height: | 973 km |
| right ascension of ascending node: | 262.0374° |
| argument of perigee: | 274.7722° |
| revolutions per day: | 13.87452557 |
| mean anomaly at epoch: | 100.9051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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