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 38342U 26145.56570169 +.00000000 +00000-0 +00000-0 0 00000
2 38342 0.0382 85.1322 0002739 337.0179 293.5509 1.00271438 06
| Epoch (UTC): | 25 May 2026 13:34:36 |
| Eccentricity: | 0.0002739 |
| inclination: | 0.0382° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 85.1322° |
| argument of perigee: | 337.0179° |
| revolutions per day: | 1.00271438 |
| mean anomaly at epoch: | 293.5509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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