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 26106.32774051 +.00000000 +00000-0 +93334-4 0 00000
2 19070 90.3327 20.3123 0188680 193.4083 288.7583 13.27808298 02
| Epoch (UTC): | 16 April 2026 07:51:56 |
| Eccentricity: | 0.0188680 |
| inclination: | 90.3327° |
| perigee height: | 1013 km |
| apogee height: | 1297 km |
| right ascension of ascending node: | 20.3123° |
| argument of perigee: | 193.4083° |
| revolutions per day: | 13.27808298 |
| mean anomaly at epoch: | 288.7583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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