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 60332U 26145.53773751 +.00000000 +00000-0 +26954-7 0 00006
2 60332 53.1602 78.4909 0001653 92.3035 267.8155 15.30188188 04
| Epoch (UTC): | 25 May 2026 12:54:20 |
| Eccentricity: | 0.0001653 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.4909° |
| argument of perigee: | 92.3035° |
| revolutions per day: | 15.30188188 |
| mean anomaly at epoch: | 267.8155° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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