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 65462U 26145.35095478 +.00000000 +00000-0 +82718-3 0 00004
2 65462 53.1581 261.9040 0001948 75.4802 284.6416 15.34412983 09
| Epoch (UTC): | 25 May 2026 08:25:22 |
| Eccentricity: | 0.0001948 |
| inclination: | 53.1581° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 261.9040° |
| argument of perigee: | 75.4802° |
| revolutions per day: | 15.34412983 |
| mean anomaly at epoch: | 284.6416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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