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 65949U 26145.61453250 +.00000000 +00000-0 +21514-3 0 00006
2 65949 51.9017 17.9230 0000917 106.3495 253.7569 14.79935197 07
| Epoch (UTC): | 25 May 2026 14:44:55 |
| Eccentricity: | 0.0000917 |
| inclination: | 51.9017° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 17.9230° |
| argument of perigee: | 106.3495° |
| revolutions per day: | 14.79935197 |
| mean anomaly at epoch: | 253.7569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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