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 57192U 26145.61833617 +.00000000 +00000-0 +36575-3 0 00009
2 57192 97.5083 208.5488 0012068 177.8405 182.2887 15.25431485 06
| Epoch (UTC): | 25 May 2026 14:50:24 |
| Eccentricity: | 0.0012068 |
| inclination: | 97.5083° |
| perigee height: | 481 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 208.5488° |
| argument of perigee: | 177.8405° |
| revolutions per day: | 15.25431485 |
| mean anomaly at epoch: | 182.2887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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