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 65154U 26145.40618187 +.00000000 +00000-0 -50981-3 0 00004
2 65154 51.8982 196.3446 0000606 334.5877 25.5055 14.79959982 03
| Epoch (UTC): | 25 May 2026 09:44:54 |
| Eccentricity: | 0.0000606 |
| inclination: | 51.8982° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 196.3446° |
| argument of perigee: | 334.5877° |
| revolutions per day: | 14.79959982 |
| mean anomaly at epoch: | 25.5055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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