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 62148U 26145.27923241 +.00000000 +00000-0 +40489-3 0 00000
2 62148 43.0021 85.5492 0001030 257.8958 102.1778 15.27590406 09
| Epoch (UTC): | 25 May 2026 06:42:05 |
| Eccentricity: | 0.0001030 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 85.5492° |
| argument of perigee: | 257.8958° |
| revolutions per day: | 15.27590406 |
| mean anomaly at epoch: | 102.1778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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