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 25159U 26087.70735439 +.00000000 +00000-0 +38032-3 0 00005
2 25159 107.9603 3.8241 0038470 107.7162 252.8183 14.35569350 04
| Epoch (UTC): | 28 March 2026 16:58:35 |
| Eccentricity: | 0.0038470 |
| inclination: | 107.9603° |
| perigee height: | 746 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 3.8241° |
| argument of perigee: | 107.7162° |
| revolutions per day: | 14.35569350 |
| mean anomaly at epoch: | 252.8183° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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