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 26107.00509529 +.00000000 +00000-0 +20831-3 0 00002
2 38735 82.4714 112.8497 0017029 197.0410 163.0100 12.42646798 07
| Epoch (UTC): | 17 April 2026 00:07:20 |
| Eccentricity: | 0.0017029 |
| inclination: | 82.4714° |
| perigee height: | 1482 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 112.8497° |
| argument of perigee: | 197.0410° |
| revolutions per day: | 12.42646798 |
| mean anomaly at epoch: | 163.0100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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