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 65488U 26145.47052322 +.00000000 +00000-0 +17719-3 0 00005
2 65488 97.4131 328.3557 0015275 105.5013 254.7905 15.10252630 03
| Epoch (UTC): | 25 May 2026 11:17:33 |
| Eccentricity: | 0.0015275 |
| inclination: | 97.4131° |
| perigee height: | 525 km |
| apogee height: | 546 km |
| right ascension of ascending node: | 328.3557° |
| argument of perigee: | 105.5013° |
| revolutions per day: | 15.10252630 |
| mean anomaly at epoch: | 254.7905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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