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 35933U 26044.67938918 +.00000000 +00000-0 +22760-3 0 00003
2 35933 98.4050 310.2822 0003990 248.0954 111.9822 14.61473462 04
| Epoch (UTC): | 13 February 2026 16:18:19 |
| Eccentricity: | 0.0003990 |
| inclination: | 98.4050° |
| perigee height: | 686 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 310.2822° |
| argument of perigee: | 248.0954° |
| revolutions per day: | 14.61473462 |
| mean anomaly at epoch: | 111.9822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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