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 15595U 26103.81971075 +.00000000 +00000-0 +56691-4 0 00009
2 15595 108.0512 307.4829 0001970 253.8329 106.2596 14.39937382 04
| Epoch (UTC): | 13 April 2026 19:40:23 |
| Eccentricity: | 0.0001970 |
| inclination: | 108.0512° |
| perigee height: | 757 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 307.4829° |
| argument of perigee: | 253.8329° |
| revolutions per day: | 14.39937382 |
| mean anomaly at epoch: | 106.2596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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