X Report 26 Jul 2025
This week's SpaceX developments include notable upcoming missions, with a Starlink launch on the horizon and Crew Dragon's readiness for the next astronaut mission.
Launch Date
May 3, 2024
Launch Site
Wenchang Space Launch Site, Hainan Province
Launch Pad
LC101
Launch Vehicle
Long March 5
NORAD ID
59627
International Designator
2024-083A
Decay Date
Unknown
Name
Chang'e-6
Alternative Name
Chang'e-6 Guidao Qi
Type
Status
Owner
China National Space Administration (CNSA)
Country
China
Constellation
N/A
Related Satellites
Major Events
Launch on May 3, 2024; lunar landing on June 1, 2024; sample collection completed by June 3, 2024; return capsule landed in Inner Mongolia on June 25, 2024.
Length
2
Diameter
4
Span
10
Dry Mass
950
Launch Mass
3406
Shape
Cylindrical with two solar panel arrays.
Radar Cross Section
0.122
Visual Magnitude
Approximately 5.0
Color
Silver (aluminum-clad)
Material Composition
The spacecraft was constructed using aluminum and magnesium alloys to ensure structural integrity while minimizing weight.
Payload
The payload included a lander, an ascender, an orbiter, and a returner. The lander was equipped with instruments for sample collection, while the ascender transported the samples to lunar orbit for transfer to the returner.
Purpose
Lunar sample return from the far side of the Moon.
Mission
Chang'e-6 was China's second lunar sample-return mission, aiming to collect and return samples from the far side of the Moon, specifically from the South Pole-Aitken Basin. The mission successfully returned the world's first samples collected from the Moon's far side.
Manufacturer
Shanghai Academy of Spaceflight Technology (SAST)
Life Expectancy
The mission lasted approximately 53 days, from launch on May 3, 2024, to the return of the sample capsule on June 25, 2024.
Bus
CE-6
Configuration
Lunar Sample Return
Motor
Main engine for lunar orbit insertion and descent, ascent engine for returning lunar samples to orbit.
Equipment
The Chang'e-6 mission carried several international payloads, including a RadoN detector from France, a lunar surface negative ion analyzer from the European Space Agency, a laser angle reflector from Italy, and a cube satellite from Pakistan.
Power System
The spacecraft utilized deployable solar arrays and batteries to power its systems during various mission phases.
ADCS
Three-axis stabilized using star trackers and gyroscopes.
Transmitter Frequency
X-band for communication with Earth; S-band for communication between modules.
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