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 65348U 26145.55982537 +.00000000 +00000-0 +54048-3 0 00005
2 65348 53.1615 209.8469 0001690 88.6070 271.5125 15.30214191 02
| Epoch (UTC): | 25 May 2026 13:26:08 |
| Eccentricity: | 0.0001690 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.8469° |
| argument of perigee: | 88.6070° |
| revolutions per day: | 15.30214191 |
| mean anomaly at epoch: | 271.5125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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