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 42841U 26145.26045973 +.00000000 +00000-0 +60244-3 0 00005
2 42841 97.3995 330.2733 0004959 74.2931 285.8858 15.32784587 01
| Epoch (UTC): | 25 May 2026 06:15:03 |
| Eccentricity: | 0.0004959 |
| inclination: | 97.3995° |
| perigee height: | 464 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 330.2733° |
| argument of perigee: | 74.2931° |
| revolutions per day: | 15.32784587 |
| mean anomaly at epoch: | 285.8858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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