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 03338U 26104.09179728 +.00000000 +00000-0 +10010-3 0 00001
2 03338 80.6583 135.9341 1130378 71.7648 300.2974 12.23562855 05
| Epoch (UTC): | 14 April 2026 02:12:11 |
| Eccentricity: | 0.1130378 |
| inclination: | 80.6583° |
| perigee height: | 678 km |
| apogee height: | 2476 km |
| right ascension of ascending node: | 135.9341° |
| argument of perigee: | 71.7648° |
| revolutions per day: | 12.23562855 |
| mean anomaly at epoch: | 300.2974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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