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 47628U 26145.49984128 +.00000000 +00000-0 +14863-3 0 00008
2 47628 53.1604 67.7474 0001601 89.1939 270.9246 15.31704242 09
| Epoch (UTC): | 25 May 2026 11:59:46 |
| Eccentricity: | 0.0001601 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 67.7474° |
| argument of perigee: | 89.1939° |
| revolutions per day: | 15.31704242 |
| mean anomaly at epoch: | 270.9246° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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