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 38734U 26104.17822500 +.00000000 +00000-0 -92167-4 0 00006
2 38734 82.4698 104.9089 0016028 197.4684 162.5847 12.44900002 06
| Epoch (UTC): | 14 April 2026 04:16:38 |
| Eccentricity: | 0.0016028 |
| inclination: | 82.4698° |
| perigee height: | 1473 km |
| apogee height: | 1499 km |
| right ascension of ascending node: | 104.9089° |
| argument of perigee: | 197.4684° |
| revolutions per day: | 12.44900002 |
| mean anomaly at epoch: | 162.5847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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