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 62120U 26145.17942302 +.00000000 +00000-0 +84090-3 0 00004
2 62120 43.0028 64.5062 0001575 276.4512 83.6160 15.27597911 09
| Epoch (UTC): | 25 May 2026 04:18:22 |
| Eccentricity: | 0.0001575 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 64.5062° |
| argument of perigee: | 276.4512° |
| revolutions per day: | 15.27597911 |
| mean anomaly at epoch: | 83.6160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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