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 62151U 26145.23311957 +.00000000 +00000-0 +69968-3 0 00008
2 62151 43.0032 86.0546 0001880 265.2377 94.8260 15.27597507 04
| Epoch (UTC): | 25 May 2026 05:35:41 |
| Eccentricity: | 0.0001880 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 86.0546° |
| argument of perigee: | 265.2377° |
| revolutions per day: | 15.27597507 |
| mean anomaly at epoch: | 94.8260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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