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 23342U 26106.76238559 +.00000000 +00000-0 +55096-4 0 00006
2 23342 97.6673 127.5662 0000955 86.2924 273.8400 14.85008851 07
| Epoch (UTC): | 16 April 2026 18:17:50 |
| Eccentricity: | 0.0000955 |
| inclination: | 97.6673° |
| perigee height: | 613 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 127.5662° |
| argument of perigee: | 86.2924° |
| revolutions per day: | 14.85008851 |
| mean anomaly at epoch: | 273.8400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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