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 62312U 26145.56269874 +.00000000 +00000-0 +48410-3 0 00002
2 62312 53.1596 196.8441 0000722 82.5887 277.5198 15.34426679 03
| Epoch (UTC): | 25 May 2026 13:30:17 |
| Eccentricity: | 0.0000722 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 196.8441° |
| argument of perigee: | 82.5887° |
| revolutions per day: | 15.34426679 |
| mean anomaly at epoch: | 277.5198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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