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 65134U 26145.43857456 +.00000000 +00000-0 +26539-3 0 00000
2 65134 51.8963 166.2499 0000469 76.7284 283.3731 14.79937797 03
| Epoch (UTC): | 25 May 2026 10:31:32 |
| Eccentricity: | 0.0000469 |
| inclination: | 51.8963° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 166.2499° |
| argument of perigee: | 76.7284° |
| revolutions per day: | 14.79937797 |
| mean anomaly at epoch: | 283.3731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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