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 19046U 26159.22900264 +.00000000 +00000-0 +19640-3 0 00004
2 19046 97.5253 142.2794 0023652 278.6984 81.1572 15.20772910 02
| Epoch (UTC): | 08 June 2026 05:29:45 |
| Eccentricity: | 0.0023652 |
| inclination: | 97.5253° |
| perigee height: | 487 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 142.2794° |
| argument of perigee: | 278.6984° |
| revolutions per day: | 15.20772910 |
| mean anomaly at epoch: | 81.1572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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