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 65788U 26145.46471104 +.00000000 +00000-0 +18148-3 0 00007
2 65788 51.9010 63.5982 0000947 103.2737 256.8331 14.79927363 07
| Epoch (UTC): | 25 May 2026 11:09:11 |
| Eccentricity: | 0.0000947 |
| inclination: | 51.9010° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 63.5982° |
| argument of perigee: | 103.2737° |
| revolutions per day: | 14.79927363 |
| mean anomaly at epoch: | 256.8331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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