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 38101U 26153.86238593 +.00000000 +00000-0 +00000-0 0 00007
2 38101 8.8197 56.4946 0004924 241.3141 306.6770 1.00381181 09
| Epoch (UTC): | 02 June 2026 20:41:50 |
| Eccentricity: | 0.0004924 |
| inclination: | 8.8197° |
| perigee height: | 35735 km |
| apogee height: | 35777 km |
| right ascension of ascending node: | 56.4946° |
| argument of perigee: | 241.3141° |
| revolutions per day: | 1.00381181 |
| mean anomaly at epoch: | 306.6770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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