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 65146U 26145.42238400 +.00000000 +00000-0 +30147-3 0 00004
2 65146 51.9006 181.3122 0000313 41.7470 318.3516 14.79942191 07
| Epoch (UTC): | 25 May 2026 10:08:13 |
| Eccentricity: | 0.0000313 |
| inclination: | 51.9006° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 181.3122° |
| argument of perigee: | 41.7470° |
| revolutions per day: | 14.79942191 |
| mean anomaly at epoch: | 318.3516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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