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 19039U 26039.89849304 +.00000000 +00000-0 +66263-4 0 00007
2 19039 74.0448 238.7009 0023384 345.9213 14.1287 14.39937648 04
| Epoch (UTC): | 08 February 2026 21:33:49 |
| Eccentricity: | 0.0023384 |
| inclination: | 74.0448° |
| perigee height: | 742 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 238.7009° |
| argument of perigee: | 345.9213° |
| revolutions per day: | 14.39937648 |
| mean anomaly at epoch: | 14.1287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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