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 65490U 26145.25786815 +.00000000 +00000-0 +18135-3 0 00008
2 65490 97.4108 332.5233 0016153 91.3710 268.9378 15.24304229 08
| Epoch (UTC): | 25 May 2026 06:11:19 |
| Eccentricity: | 0.0016153 |
| inclination: | 97.4108° |
| perigee height: | 482 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 332.5233° |
| argument of perigee: | 91.3710° |
| revolutions per day: | 15.24304229 |
| mean anomaly at epoch: | 268.9378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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