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 65034U 26144.81415646 +.00000000 +00000-0 +34325-3 0 00003
2 65034 53.1611 300.6946 0001238 81.0464 279.0677 15.30204180 04
| Epoch (UTC): | 24 May 2026 19:32:23 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.6946° |
| argument of perigee: | 81.0464° |
| revolutions per day: | 15.30204180 |
| mean anomaly at epoch: | 279.0677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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