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 33496U 26102.01129205 +.00000000 +00000-0 +62312-4 0 00007
2 33496 98.1443 6.3597 0004896 216.6897 143.3977 14.74961874 07
| Epoch (UTC): | 12 April 2026 00:16:15 |
| Eccentricity: | 0.0004896 |
| inclination: | 98.1443° |
| perigee height: | 642 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 6.3597° |
| argument of perigee: | 216.6897° |
| revolutions per day: | 14.74961874 |
| mean anomaly at epoch: | 143.3977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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