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 33397U 26087.94181306 +.00000000 +00000-0 +34232-4 0 00001
2 33397 98.7267 224.4078 0337148 235.2827 235.7084 13.92007369 07
| Epoch (UTC): | 28 March 2026 22:36:12 |
| Eccentricity: | 0.0337148 |
| inclination: | 98.7267° |
| perigee height: | 675 km |
| apogee height: | 1168 km |
| right ascension of ascending node: | 224.4078° |
| argument of perigee: | 235.2827° |
| revolutions per day: | 13.92007369 |
| mean anomaly at epoch: | 235.7084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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