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: 2 days ago
TLE from 2 days ago
0 RCM 3
1 44323U 19033B 25259.50356975 .00001152 00000-0 11745-3 0 9995
2 44323 97.7597 265.9705 0001493 91.3764 268.7626 14.92592748341278Epoch: 2025-09-16T12:05Z
TLE epoch observation values (Epoch: 2025-09-16T12:05:08.426Z)
Latitude
-0.00004°
Longitude
88.99247°
Altitude
592.92 km
Speed
7.563 km/s
True Right ascension
17h 43m 52s
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
22:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.912 km
Perigee altitude
585.833 km
Semi-major axis
6,965.009 km
Eccentricity
0.00015
Inclination
97.7597°
RAAN
265.9705°
Arg. of periapsis
91.3764°
True anomaly
268.7455°
Mean anomaly
268.7626°
Eccentric anomaly
268.75405°
Mean motion
3.73388 °/min
Orbital period
96.41 mins
BSTAR
0.00011745
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 12:55:56.377Z | 33.902° NE | 2025-09-18 12:58:56.377Z | 100.059° ESE | 32.733° | 2025-09-18 13:01:56.377Z | 163.619° S |
| 4 mins | 2025-09-18 23:46:56.377Z | 102.616° ESE | 2025-09-18 23:48:56.377Z | 57.538° ENE | 22.927° | 2025-09-18 23:50:56.377Z | 22.299° NNE |
| 5 mins | 2025-09-19 01:21:56.377Z | 225.66° WSW | 2025-09-19 01:23:56.377Z | 265.713° W | 22.186° | 2025-09-19 01:26:56.377Z | 316.6° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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