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 65361U 26145.39266071 +.00000000 +00000-0 +21775-3 0 00001
2 65361 53.1595 171.5505 0001204 83.5529 276.5609 15.30198802 06
| Epoch (UTC): | 25 May 2026 09:25:25 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.5505° |
| argument of perigee: | 83.5529° |
| revolutions per day: | 15.30198802 |
| mean anomaly at epoch: | 276.5609° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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