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 65088U 26145.09472220 +.00000000 +00000-0 +60875-3 0 00003
2 65088 53.1599 32.0597 0001220 95.2031 264.9109 15.30223183 01
| Epoch (UTC): | 25 May 2026 02:16:23 |
| Eccentricity: | 0.0001220 |
| inclination: | 53.1599° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 32.0597° |
| argument of perigee: | 95.2031° |
| revolutions per day: | 15.30223183 |
| mean anomaly at epoch: | 264.9109° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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