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 62671U 26145.58478462 +.00000000 +00000-0 +10644-3 0 00005
2 62671 97.3989 224.5692 0006684 63.0493 297.1425 15.20878609 04
| Epoch (UTC): | 25 May 2026 14:02:05 |
| Eccentricity: | 0.0006684 |
| inclination: | 97.3989° |
| perigee height: | 499 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 224.5692° |
| argument of perigee: | 63.0493° |
| revolutions per day: | 15.20878609 |
| mean anomaly at epoch: | 297.1425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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