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 65148U 26145.41428160 +.00000000 +00000-0 -95658-4 0 00009
2 65148 51.8982 188.8591 0000682 96.2938 263.8102 14.79929758 05
| Epoch (UTC): | 25 May 2026 09:56:33 |
| Eccentricity: | 0.0000682 |
| inclination: | 51.8982° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 188.8591° |
| argument of perigee: | 96.2938° |
| revolutions per day: | 14.79929758 |
| mean anomaly at epoch: | 263.8102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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