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 42832U 26104.16016788 +.00000000 +00000-0 +12661-3 0 00001
2 42832 97.4098 266.9996 0009409 340.8329 19.2544 15.07637814 03
| Epoch (UTC): | 14 April 2026 03:50:38 |
| Eccentricity: | 0.0009409 |
| inclination: | 97.4098° |
| perigee height: | 537 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 266.9996° |
| argument of perigee: | 340.8329° |
| revolutions per day: | 15.07637814 |
| mean anomaly at epoch: | 19.2544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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