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 26032.28717660 +.00000000 +00000-0 +26254-3 0 00008
2 35933 98.4063 297.6918 0004214 298.5729 61.5047 14.61438185 04
| Epoch (UTC): | 01 February 2026 06:53:32 |
| Eccentricity: | 0.0004214 |
| inclination: | 98.4063° |
| perigee height: | 686 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 297.6918° |
| argument of perigee: | 298.5729° |
| revolutions per day: | 14.61438185 |
| mean anomaly at epoch: | 61.5047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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