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 63713U 26145.48175391 +.00000000 +00000-0 +69107-3 0 00005
2 63713 53.1595 222.3788 0001277 95.5217 264.5931 15.31705832 03
| Epoch (UTC): | 25 May 2026 11:33:43 |
| Eccentricity: | 0.0001277 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 222.3788° |
| argument of perigee: | 95.5217° |
| revolutions per day: | 15.31705832 |
| mean anomaly at epoch: | 264.5931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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