IRIDIUM 179, 56730
Orbit data source: Space-Track
IRIDIUM 179, 56730 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 20 May 2023 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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56730 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NGIS 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: 2 days ago
TLE from 2 days ago
0 IRIDIUM 179
1 56730U 23068W 26171.34838329 .00000700 00000-0 88708-4 0 9999
2 56730 86.6772 33.0280 0002470 88.2467 271.9038 14.80235509166834Epoch: 2026-06-20T08:21Z
TLE epoch observation values (Epoch: 2026-06-20T08:21:40.316Z)
Latitude
0.00004°
Longitude
-0.95428°
Altitude
631.643 km
Speed
7.543 km/s
True Right ascension
02h 12m 06s
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
21:31:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.205 km
Perigee altitude
623.745 km
Semi-major axis
7,003.612 km
Eccentricity
0.00025
Inclination
86.6772°
RAAN
33.028°
Arg. of periapsis
88.2467°
True anomaly
271.87551°
Mean anomaly
271.9038°
Eccentric anomaly
271.88966°
Mean motion
3.70305 °/min
Orbital period
97.22 mins
BSTAR
0.000088708
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Other satellites on launch #68 in the year 2023 (2023-05-20 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 179 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 14:03:01.450Z | 109.879° ESE | 2026-06-22 14:05:01.450Z | 81.847° E | 13.954° | 2026-06-22 14:07:01.450Z | 52.879° ENE |
| 6 mins | 2026-06-22 15:40:01.450Z | 215.406° SW | 2026-06-22 15:42:01.450Z | 263.856° W | 35.001° | 2026-06-22 15:46:01.450Z | 346.787° N |
| 5 mins | 2026-06-23 01:51:01.450Z | 45.523° ENE | 2026-06-23 01:53:01.450Z | 79.589° E | 18.966° | 2026-06-23 01:56:01.450Z | 124.847° SE |
| 6 mins | 2026-06-23 03:28:01.450Z | 326.804° NNW | 2026-06-23 03:31:01.450Z | 263.288° W | 27.423° | 2026-06-23 03:34:01.450Z | 215.544° SW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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