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 65216U 26145.26824638 +.00000000 +00000-0 +72123-3 0 00008
2 65216 53.1574 156.4141 0000934 91.2408 268.8701 15.34418465 02
| Epoch (UTC): | 25 May 2026 06:26:16 |
| Eccentricity: | 0.0000934 |
| inclination: | 53.1574° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 156.4141° |
| argument of perigee: | 91.2408° |
| revolutions per day: | 15.34418465 |
| mean anomaly at epoch: | 268.8701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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