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 42844U 26145.44883661 +.00000000 +00000-0 +47667-3 0 00006
2 42844 97.3733 320.1024 0005702 97.8301 262.3583 15.23948442 01
| Epoch (UTC): | 25 May 2026 10:46:19 |
| Eccentricity: | 0.0005702 |
| inclination: | 97.3733° |
| perigee height: | 490 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 320.1024° |
| argument of perigee: | 97.8301° |
| revolutions per day: | 15.23948442 |
| mean anomaly at epoch: | 262.3583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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