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 65713U 26145.15221189 +.00000000 +00000-0 +18814-3 0 00007
2 65713 49.9872 55.3047 0012033 138.6670 221.5181 14.83182323 02
| Epoch (UTC): | 25 May 2026 03:39:11 |
| Eccentricity: | 0.0012033 |
| inclination: | 49.9872° |
| perigee height: | 611 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 55.3047° |
| argument of perigee: | 138.6670° |
| revolutions per day: | 14.83182323 |
| mean anomaly at epoch: | 221.5181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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