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 65930U 26145.35528569 +.00000000 +00000-0 +12717-3 0 00008
2 65930 53.1573 169.7386 0001104 78.4695 281.6430 15.30188492 09
| Epoch (UTC): | 25 May 2026 08:31:36 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1573° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.7386° |
| argument of perigee: | 78.4695° |
| revolutions per day: | 15.30188492 |
| mean anomaly at epoch: | 281.6430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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