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 63947U 26145.55446288 +.00000000 +00000-0 +23337-3 0 00003
2 63947 70.0012 80.7512 0002575 269.1940 90.8924 14.98341304 03
| Epoch (UTC): | 25 May 2026 13:18:25 |
| Eccentricity: | 0.0002575 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.7512° |
| argument of perigee: | 269.1940° |
| revolutions per day: | 14.98341304 |
| mean anomaly at epoch: | 90.8924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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