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 33495U 26038.71629852 +.00000000 +00000-0 +10171-3 0 00009
2 33495 98.1328 303.8979 0009037 84.8291 275.3948 14.74679193 06
| Epoch (UTC): | 07 February 2026 17:11:28 |
| Eccentricity: | 0.0009037 |
| inclination: | 98.1328° |
| perigee height: | 640 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 303.8979° |
| argument of perigee: | 84.8291° |
| revolutions per day: | 14.74679193 |
| mean anomaly at epoch: | 275.3948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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