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 42992U 26145.38257181 +.00000000 +00000-0 +27937-3 0 00003
2 42992 97.4536 282.7706 0001966 190.4014 169.7188 15.33999640 04
| Epoch (UTC): | 25 May 2026 09:10:54 |
| Eccentricity: | 0.0001966 |
| inclination: | 97.4536° |
| perigee height: | 463 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 282.7706° |
| argument of perigee: | 190.4014° |
| revolutions per day: | 15.33999640 |
| mean anomaly at epoch: | 169.7188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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