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 60128U 26145.38816119 +.00000000 +00000-0 +30026-4 0 00000
2 60128 53.1609 30.1565 0001063 91.1419 268.9705 15.31702720 03
| Epoch (UTC): | 25 May 2026 09:18:57 |
| Eccentricity: | 0.0001063 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 30.1565° |
| argument of perigee: | 91.1419° |
| revolutions per day: | 15.31702720 |
| mean anomaly at epoch: | 268.9705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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