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 67154U 26145.51873117 +.00000000 +00000-0 +46451-3 0 00000
2 67154 51.8999 75.9054 0000822 75.9734 284.1320 14.79910548 01
| Epoch (UTC): | 25 May 2026 12:26:58 |
| Eccentricity: | 0.0000822 |
| inclination: | 51.8999° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 75.9054° |
| argument of perigee: | 75.9734° |
| revolutions per day: | 14.79910548 |
| mean anomaly at epoch: | 284.1320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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