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 38735U 26155.23215898 +.00000000 +00000-0 +19921-3 0 00001
2 38735 82.4760 82.7696 0018615 94.5605 265.7602 12.42648795 09
| Epoch (UTC): | 04 June 2026 05:34:18 |
| Eccentricity: | 0.0018615 |
| inclination: | 82.4760° |
| perigee height: | 1481 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 82.7696° |
| argument of perigee: | 94.5605° |
| revolutions per day: | 12.42648795 |
| mean anomaly at epoch: | 265.7602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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