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 62152U 26145.53130484 +.00000000 +00000-0 +63414-3 0 00006
2 62152 43.0014 87.4539 0000643 4.9146 355.1712 15.27590098 03
| Epoch (UTC): | 25 May 2026 12:45:04 |
| Eccentricity: | 0.0000643 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 87.4539° |
| argument of perigee: | 4.9146° |
| revolutions per day: | 15.27590098 |
| mean anomaly at epoch: | 355.1712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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