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IRIDIUM 175, 43928

Orbit data source: Space-Track

IRIDIUM 175, 43928 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 11 Jan 2019 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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IRIDIUM 175 details

Identifier	43928, 2019-002G
Orbit	LEO
Last TLE update	9 hours ago
Origin	Iridium (US)
Manufacturer	NGIS SSG Gilbert
Mission	Operational Commercial Communications
Bus & Motor	ELITEBUS, Unknown motor
Mass	860 kg wet, 700 kg dry
Launch date (UTC)	2019-01-11 (6 years ago)
Launch vehicle	FALCON 9
Launch site	Air Force Western Test Range (AFWTR)
Object type	Payload Rocket body Debris
Shape & HBR	Trap Box + 2 Pan, 9.4 m
Radar Cross Section	14.423 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 IRIDIUM 175
1 43928U 19002G   24361.25725313  .00000982  00000-0  15181-3 0  9990
2 43928  86.1522 180.7161 0000856 127.1231 233.0064 14.72248841320095

Epoch: 2024-12-26T06:10Z

Definitive object data (Epoch: 2024-12-26T06:10:26.67Z)

Latitude	-0.00001°
Longitude	-7.13427°
Altitude	657.362 km
Speed	7.528 km/s
True Right ascension	12h 02m 51s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	72.94533°
Longitude	160.09994°
Altitude	665.957 km
Speed	7.531 km/s
Apparent Right ascension	01h 19m 08s
Apparent Declination	22° 00' 23"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	14:10:41
Azimuth	13.411° NNE
Elevation	-26.92°
Doppler factor	1

Orbital elements

Apogee altitude	651.416 km
Perigee altitude	650.213 km
Semi-major axis	7,028.951 km
Eccentricity	0.0000856
Inclination	86.1522°
RAAN	180.7161°
Arg. of periapsis	127.1231°
True anomaly	232.99857°
Mean anomaly	233.0064°
Eccentric anomaly	233.00248°
Mean motion	3.68305 °/min
BSTAR	0.00015181
Orbital period	97.75 mins

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Other satellites on launch #2 in the year 2019 (2019-01-11 UTC)

IRIDIUM 175 Visibility forecast

Observer location: undefined°, undefined

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
7 mins	2024-12-27 00:41:47.082Z	343.258° N	2024-12-27 00:44:47.082Z	286.829° WNW	38.397°	2024-12-27 00:48:47.082Z	197.219° SSW
4 mins	2024-12-27 11:41:47.082Z	104.424° ESE	2024-12-27 11:42:47.082Z	88.632° E	16.918°	2024-12-27 11:45:47.082Z	43.958° NE
6 mins	2024-12-27 13:18:47.082Z	224.571° SW	2024-12-27 13:20:47.082Z	269.31° W	31.553°	2024-12-27 13:24:47.082Z	343.689° N

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Check out IRIDIUM 175, 43928 on other resources

View IRIDIUM 175, 43928 on NASA - NSSDCA Website

View IRIDIUM 175, 43928 on Heavens-Above

View IRIDIUM 175, 43928 on Keep Track

View IRIDIUM 175, 43928 on Celestrak

View IRIDIUM 175, 43928 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.