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 62114U 26145.13623653 +.00000000 +00000-0 +35902-3 0 00006
2 62114 43.0021 49.4716 0001573 262.5709 97.4964 15.27590215 00
| Epoch (UTC): | 25 May 2026 03:16:10 |
| Eccentricity: | 0.0001573 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 49.4716° |
| argument of perigee: | 262.5709° |
| revolutions per day: | 15.27590215 |
| mean anomaly at epoch: | 97.4964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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