IRIDIUM 130, 43073
Orbit data source: Space-Track
IRIDIUM 130, 43073 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 23 Dec 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft 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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43073 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 IRIDIUM 130
1 43073U 17083D 25317.24970196 .00000558 00000-0 19201-3 0 9996
2 43073 86.3990 52.5120 0001776 100.2469 259.8927 14.34223233413166Epoch: 2025-11-13T05:59Z
TLE epoch observation values (Epoch: 2025-11-13T05:59:34.249Z)
Latitude
-0.00003°
Longitude
-89.99096°
Altitude
780.923 km
Speed
7.463 km/s
True Right ascension
03h 30m 02s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:49:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.884 km
Perigee altitude
773.343 km
Semi-major axis
7,152.75 km
Eccentricity
0.00018
Inclination
86.399°
RAAN
52.512°
Arg. of periapsis
100.2469°
True anomaly
259.87267°
Mean anomaly
259.8927°
Eccentric anomaly
259.88268°
Mean motion
3.58784 °/min
Orbital period
100.34 mins
BSTAR
0.00019201
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Other satellites on launch #83 in the year 2017 (2017-12-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 130 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-11-13 18:17:29.397Z | 9.716° NNE | 2025-11-13 18:21:29.397Z | 71.403° E | 38.576° | 2025-11-13 18:26:29.397Z | 160.839° S |
| 4 mins | 2025-11-13 20:00:29.397Z | 301.08° NW | 2025-11-13 20:01:29.397Z | 287.899° WNW | 15.644° | 2025-11-13 20:04:29.397Z | 249.419° W |
| 8 mins | 2025-11-14 07:14:29.397Z | 193.643° SSW | 2025-11-14 07:17:29.397Z | 252.661° W | 43.061° | 2025-11-14 07:22:29.397Z | 357.17° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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