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 62664U 26145.60041051 +.00000000 +00000-0 +39561-3 0 00009
2 62664 97.3987 220.6647 0007319 269.1244 90.9152 15.18371990 04
| Epoch (UTC): | 25 May 2026 14:24:35 |
| Eccentricity: | 0.0007319 |
| inclination: | 97.3987° |
| perigee height: | 506 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 220.6647° |
| argument of perigee: | 269.1244° |
| revolutions per day: | 15.18371990 |
| mean anomaly at epoch: | 90.9152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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