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 38012U 26114.27885578 +.00000000 +00000-0 +48010-4 0 00008
2 38012 98.1981 190.1009 0001066 77.9513 13.0810 14.58535617 05
| Epoch (UTC): | 24 April 2026 06:41:33 |
| Eccentricity: | 0.0001066 |
| inclination: | 98.1981° |
| perigee height: | 697 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 190.1009° |
| argument of perigee: | 77.9513° |
| revolutions per day: | 14.58535617 |
| mean anomaly at epoch: | 13.0810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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