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 14033U 26160.05443209 +.00000000 +00000-0 +43554-4 0 00001
2 14033 82.5054 145.6888 0018499 90.5253 269.8083 14.86263062 06
| Epoch (UTC): | 09 June 2026 01:18:22 |
| Eccentricity: | 0.0018499 |
| inclination: | 82.5054° |
| perigee height: | 597 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 145.6888° |
| argument of perigee: | 90.5253° |
| revolutions per day: | 14.86263062 |
| mean anomaly at epoch: | 269.8083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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