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 15202U 26088.00749514 +.00000000 +00000-0 +11035-3 0 00000
2 15202 28.9005 174.5760 1982871 131.1512 247.7827 10.82241846 09
| Epoch (UTC): | 29 March 2026 00:10:47 |
| Eccentricity: | 0.1982871 |
| inclination: | 28.9005° |
| perigee height: | 543 km |
| apogee height: | 3967 km |
| right ascension of ascending node: | 174.5760° |
| argument of perigee: | 131.1512° |
| revolutions per day: | 10.82241846 |
| mean anomaly at epoch: | 247.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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