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 63772U 26145.39697142 +.00000000 +00000-0 +92579-4 0 00003
2 63772 98.0744 333.0438 0001417 90.0658 270.0709 14.67535428 04
| Epoch (UTC): | 25 May 2026 09:31:38 |
| Eccentricity: | 0.0001417 |
| inclination: | 98.0744° |
| perigee height: | 668 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 333.0438° |
| argument of perigee: | 90.0658° |
| revolutions per day: | 14.67535428 |
| mean anomaly at epoch: | 270.0709° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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