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 63715U 26145.51398477 +.00000000 +00000-0 +44547-3 0 00004
2 63715 53.1574 222.5746 0001119 77.3211 282.7915 15.30207758 02
| Epoch (UTC): | 25 May 2026 12:20:08 |
| Eccentricity: | 0.0001119 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.5746° |
| argument of perigee: | 77.3211° |
| revolutions per day: | 15.30207758 |
| mean anomaly at epoch: | 282.7915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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