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 35951U 26044.87990003 +.00000000 +00000-0 +16230-3 0 00003
2 35951 98.8921 25.9956 0010076 239.3697 120.6483 14.14819649 02
| Epoch (UTC): | 13 February 2026 21:07:03 |
| Eccentricity: | 0.0010076 |
| inclination: | 98.8921° |
| perigee height: | 836 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 25.9956° |
| argument of perigee: | 239.3697° |
| revolutions per day: | 14.14819649 |
| mean anomaly at epoch: | 120.6483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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