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 65478U 26145.33784044 +.00000000 +00000-0 +95753-3 0 00006
2 65478 53.1592 261.8151 0001216 76.5067 283.6070 15.31731192 01
| Epoch (UTC): | 25 May 2026 08:06:29 |
| Eccentricity: | 0.0001216 |
| inclination: | 53.1592° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 261.8151° |
| argument of perigee: | 76.5067° |
| revolutions per day: | 15.31731192 |
| mean anomaly at epoch: | 283.6070° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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