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 38736U 26145.18461708 +.00000000 +00000-0 -79714-4 0 00006
2 38736 82.4779 85.1825 0026306 101.7776 258.6258 12.43903187 05
| Epoch (UTC): | 25 May 2026 04:25:50 |
| Eccentricity: | 0.0026306 |
| inclination: | 82.4779° |
| perigee height: | 1469 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 85.1825° |
| argument of perigee: | 101.7776° |
| revolutions per day: | 12.43903187 |
| mean anomaly at epoch: | 258.6258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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