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 19419U 26156.37857086 +.00000000 +00000-0 +13029-3 0 00009
2 19419 90.0415 20.9169 0097956 107.6372 64.5772 13.42656693 00
| Epoch (UTC): | 05 June 2026 09:05:08 |
| Eccentricity: | 0.0097956 |
| inclination: | 90.0415° |
| perigee height: | 1026 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 20.9169° |
| argument of perigee: | 107.6372° |
| revolutions per day: | 13.42656693 |
| mean anomaly at epoch: | 64.5772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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