RCM 2, 44324
Orbit data source: Space-Track
RCM 2, 44324 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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44324 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: 7 hours ago
TLE from 7 hours ago
0 RCM 2
1 44324U 19033C 25317.98386762 .00001403 00000-0 14186-3 0 9991
2 44324 97.7595 323.5599 0001505 87.8784 272.2607 14.92595030349987Epoch: 2025-11-13T23:36Z
TLE epoch observation values (Epoch: 2025-11-13T23:36:46.162Z)
Latitude
-0.00007°
Longitude
-83.96632°
Altitude
592.849 km
Speed
7.564 km/s
True Right ascension
21h 34m 14s
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
03:01:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.914 km
Perigee altitude
585.817 km
Semi-major axis
6,965.002 km
Eccentricity
0.00015
Inclination
97.7595°
RAAN
323.5599°
Arg. of periapsis
87.8784°
True anomaly
272.24347°
Mean anomaly
272.2607°
Eccentric anomaly
272.25208°
Mean motion
3.73389 °/min
Orbital period
96.41 mins
BSTAR
0.00014186
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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 2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-14 13:03:28.882Z | 27.17° NE | 2025-11-14 13:06:28.882Z | 89.402° E | 37.276° | 2025-11-14 13:10:28.882Z | 175.15° S |
| 5 mins | 2025-11-14 23:54:28.882Z | 111.574° ESE | 2025-11-14 23:56:28.882Z | 61.079° ENE | 27.006° | 2025-11-14 23:59:28.882Z | 10.874° NNE |
| 4 mins | 2025-11-15 01:30:28.882Z | 242.64° WSW | 2025-11-15 01:31:28.882Z | 261.54° W | 18.592° | 2025-11-15 01:34:28.882Z | 310.831° NW |
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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