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 63709U 26145.58879457 +.00000000 +00000-0 +32076-3 0 00000
2 63709 53.1589 222.3368 0000448 106.4029 253.7021 15.30205617 02
| Epoch (UTC): | 25 May 2026 14:07:51 |
| Eccentricity: | 0.0000448 |
| inclination: | 53.1589° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.3368° |
| argument of perigee: | 106.4029° |
| revolutions per day: | 15.30205617 |
| mean anomaly at epoch: | 253.7021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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