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 19070U 26106.25489941 +.00000000 +00000-0 +12320-3 0 00008
2 19070 90.3325 20.3099 0188670 193.5922 300.5897 13.27808442 06
| Epoch (UTC): | 16 April 2026 06:07:03 |
| Eccentricity: | 0.0188670 |
| inclination: | 90.3325° |
| perigee height: | 1013 km |
| apogee height: | 1297 km |
| right ascension of ascending node: | 20.3099° |
| argument of perigee: | 193.5922° |
| revolutions per day: | 13.27808442 |
| mean anomaly at epoch: | 300.5897° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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