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 40019U 26156.63001992 +.00000000 +00000-0 +78329-4 0 00000
2 40019 97.9637 283.8482 0077734 311.3730 48.0809 14.70872336 08
| Epoch (UTC): | 05 June 2026 15:07:13 |
| Eccentricity: | 0.0077734 |
| inclination: | 97.9637° |
| perigee height: | 604 km |
| apogee height: | 713 km |
| right ascension of ascending node: | 283.8482° |
| argument of perigee: | 311.3730° |
| revolutions per day: | 14.70872336 |
| mean anomaly at epoch: | 48.0809° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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