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Today's highlights include China's launch of the Shijian-25 for on-orbit refueling tests, major Pentagon contracts for solid rocket motors and hypersonic testing, and the US Space Force's record-setting year of launches.
NUSAT-39 (TIKVAH ALPER) (56201)
COSPAR: 2023-054Z | Alt Name: Tikvah Alper
Image
Additional Sources
Launch Details
Orbital Elements
NORAD ID
56201
International Designator
2023-054Z
Epoch
Sun, 19 Jul 2026 18:22:10 GMT
Apogee
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Perigee
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Inclination
97.31°
Right Ascension
110.85°
Eccentricity
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Argument of Perigee
286.17°
Period
93.01 min
Mean Motion
15.48 rev/day
Latitude
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Longitude
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Altitude
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Velocity
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Polar Plot
3D Visualization
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Basic Satellite Info
Name
NUSAT-39 (TIKVAH ALPER)
Alternative Name
Tikvah Alper
Type
Payload
Status
Operational
Owner
URUGUS
Country
Uruguay
Constellation
N/A
Related Satellites
Major Events
N/A
Latest TLEs
1 56201U 23054Z 26200.76539615 .00015992 00000+0 30580-3 0 9994
2 56201 97.3078 110.8510 0001446 286.1660 73.9431 15.48165515183493
Source: Celestrak
Summary
NUSAT-39 (TIKVAH ALPER) is an Earth observation satellite, also known as Alt Name Tikvah Alper, launched on April 15, 2023, from AFWTR Launch Site at SLC4E using a Falcon 9 launch vehicle. The spacecraft, manufactured by URUGUS and owned by the same entity, measures 0.813 meters in length with a diameter of 0.508 meters and a span of 0.813 meters. It has a dry mass of 38.5 kg and was launched at a mass of 41.5 kg. The satellite is configured as a Box shape equipped with an imaging payload (all) and LUSEX U/V linear transponder payload (#1). Its power supply consists of solar cells and batteries, and it is expected to operate for 3-4 years in its mission to conduct Earth observation.
Physical Characteristics
Length
0.813
Diameter
0.508
Span
0.813
Dry Mass
38.5
Launch Mass
41.5
Shape
Box
Radar Cross Section
Unknown
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
NuSat-39
Purpose
Earth observation
Mission
Earth observation
Manufacturer
URUGUS
Life Expectancy
3-4 years
Bus
Newsat V
Configuration
Unknown
Motor
None
Equipment
Imaging payload (all), LUSEX U/V linear transponder payload (#1)
Power System
Solar cells, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
Map
Next Pass
Azimuth Elevation Time (Local)
Start Azimuth
Max Elevation
Stop Azimuth
Time Until
Pass Duration
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