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 65970U 26145.29846814 +.00000000 +00000-0 +49574-3 0 00002
2 65970 51.9035 359.4686 0000635 106.8704 253.2328 14.79922994 04
| Epoch (UTC): | 25 May 2026 07:09:47 |
| Eccentricity: | 0.0000635 |
| inclination: | 51.9035° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 359.4686° |
| argument of perigee: | 106.8704° |
| revolutions per day: | 14.79922994 |
| mean anomaly at epoch: | 253.2328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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