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 42835U 26145.37014463 +.00000000 +00000-0 +17174-3 0 00004
2 42835 97.4816 302.3122 0009416 235.7229 124.3105 15.01641858 07
| Epoch (UTC): | 25 May 2026 08:53:00 |
| Eccentricity: | 0.0009416 |
| inclination: | 97.4816° |
| perigee height: | 555 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 302.3122° |
| argument of perigee: | 235.7229° |
| revolutions per day: | 15.01641858 |
| mean anomaly at epoch: | 124.3105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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