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 63756U 26145.48759212 +.00000000 +00000-0 +20346-2 0 00003
2 63756 43.0009 189.3492 0003569 272.6417 87.4042 15.70973276 05
| Epoch (UTC): | 25 May 2026 11:42:07 |
| Eccentricity: | 0.0003569 |
| inclination: | 43.0009° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 189.3492° |
| argument of perigee: | 272.6417° |
| revolutions per day: | 15.70973276 |
| mean anomaly at epoch: | 87.4042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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