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 65155U 26143.53944020 +.00000000 +00000-0 +53720-2 0 00007
2 65155 51.9002 192.2951 0001281 103.5757 256.5348 14.79627262 09
| Epoch (UTC): | 23 May 2026 12:56:47 |
| Eccentricity: | 0.0001281 |
| inclination: | 51.9002° |
| perigee height: | 630 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 192.2951° |
| argument of perigee: | 103.5757° |
| revolutions per day: | 14.79627262 |
| mean anomaly at epoch: | 256.5348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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