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 64827U 26145.50772983 +.00000000 +00000-0 +17503-3 0 00008
2 64827 51.8996 320.8770 0000707 120.8940 239.2091 14.79936843 02
| Epoch (UTC): | 25 May 2026 12:11:07 |
| Eccentricity: | 0.0000707 |
| inclination: | 51.8996° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 320.8770° |
| argument of perigee: | 120.8940° |
| revolutions per day: | 14.79936843 |
| mean anomaly at epoch: | 239.2091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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