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 38070U 26140.61056873 +.00000000 +00000-0 +00000-0 0 00000
2 38070 0.0134 324.1005 0001623 317.1680 265.2178 1.00272819 02
| Epoch (UTC): | 20 May 2026 14:39:13 |
| Eccentricity: | 0.0001623 |
| inclination: | 0.0134° |
| perigee height: | 35779 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 324.1005° |
| argument of perigee: | 317.1680° |
| revolutions per day: | 1.00272819 |
| mean anomaly at epoch: | 265.2178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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