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 42837U 26145.47205258 +.00000000 +00000-0 +54199-3 0 00009
2 42837 97.3815 326.2166 0010341 88.8915 271.3511 15.30513373 04
| Epoch (UTC): | 25 May 2026 11:19:45 |
| Eccentricity: | 0.0010341 |
| inclination: | 97.3815° |
| perigee height: | 467 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 326.2166° |
| argument of perigee: | 88.8915° |
| revolutions per day: | 15.30513373 |
| mean anomaly at epoch: | 271.3511° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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