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 47693U 26145.57127014 +.00000000 +00000-0 +43207-4 0 00007
2 47693 63.4019 256.7734 0175281 0.9030 359.2279 13.45447367 05
| Epoch (UTC): | 25 May 2026 13:42:37 |
| Eccentricity: | 0.0175281 |
| inclination: | 63.4019° |
| perigee height: | 958 km |
| apogee height: | 1220 km |
| right ascension of ascending node: | 256.7734° |
| argument of perigee: | 0.9030° |
| revolutions per day: | 13.45447367 |
| mean anomaly at epoch: | 359.2279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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