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 65030U 26145.42203977 +.00000000 +00000-0 +75907-3 0 00000
2 65030 53.1612 298.0908 0001145 123.7508 236.3602 15.30215737 03
| Epoch (UTC): | 25 May 2026 10:07:44 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.0908° |
| argument of perigee: | 123.7508° |
| revolutions per day: | 15.30215737 |
| mean anomaly at epoch: | 236.3602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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