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 63312U 26145.36054714 +.00000000 +00000-0 +12026-2 0 00009
2 63312 43.0021 162.5904 0002248 264.4451 95.6160 15.70868583 04
| Epoch (UTC): | 25 May 2026 08:39:11 |
| Eccentricity: | 0.0002248 |
| inclination: | 43.0021° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 162.5904° |
| argument of perigee: | 264.4451° |
| revolutions per day: | 15.70868583 |
| mean anomaly at epoch: | 95.6160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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