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 33499U 26039.17748453 +.00000000 +00000-0 +28445-3 0 00006
2 33499 98.1185 319.6271 0007920 359.6981 0.4226 14.82709345 07
| Epoch (UTC): | 08 February 2026 04:15:34 |
| Eccentricity: | 0.0007920 |
| inclination: | 98.1185° |
| perigee height: | 615 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 319.6271° |
| argument of perigee: | 359.6981° |
| revolutions per day: | 14.82709345 |
| mean anomaly at epoch: | 0.4226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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