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 62934U 26145.38921588 +.00000000 +00000-0 +18880-3 0 00007
2 62934 97.9680 198.6646 0002880 199.8931 160.2166 14.73314828 06
| Epoch (UTC): | 25 May 2026 09:20:28 |
| Eccentricity: | 0.0002880 |
| inclination: | 97.9680° |
| perigee height: | 648 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 198.6646° |
| argument of perigee: | 199.8931° |
| revolutions per day: | 14.73314828 |
| mean anomaly at epoch: | 160.2166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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