RCM 3, 44323
Orbit data source: Space-Track
RCM 3, 44323 is a payload satellite owned by CSA (CA) in SSO that was launched on Wed, 12 Jun 2019 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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44323 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
BALM/MAXAR
Mission
Operational Civil Radar Imaging
Bus & Motor
MAC-200, Unknown motor
Mass
1,450 kg wet, ~1,400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.5 m
Radar Cross Section
10.097 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 RCM 3
1 44323U 19033B 25303.95049465 .00001370 00000-0 13863-3 0 9992
2 44323 97.7596 309.7788 0001567 88.5429 271.5969 14.92585543347906Epoch: 2025-10-30T22:48Z
TLE epoch observation values (Epoch: 2025-10-30T22:48:42.737Z)
Latitude
-0.00011°
Longitude
-71.90118°
Altitude
592.89 km
Speed
7.564 km/s
True Right ascension
20h 39m 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
23:12:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.986 km
Perigee altitude
585.803 km
Semi-major axis
6,965.032 km
Eccentricity
0.00016
Inclination
97.7596°
RAAN
309.7788°
Arg. of periapsis
88.5429°
True anomaly
271.57895°
Mean anomaly
271.5969°
Eccentric anomaly
271.58793°
Mean motion
3.73386 °/min
Orbital period
96.41 mins
BSTAR
0.00013863
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Other satellites on launch #33 in the year 2019 (2019-06-12 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.RCM 3 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-31 13:52:32.374Z | 344.06° N | 2025-10-31 13:54:32.374Z | 289.207° WNW | 34.089° | 2025-10-31 13:57:32.374Z | 221.737° SW |
| 6 mins | 2025-11-01 00:41:32.374Z | 177.826° S | 2025-11-01 00:43:32.374Z | 211.854° SW | 41.95° | 2025-11-01 00:47:32.374Z | 342.189° 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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