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: 2 days ago
TLE from 2 days ago
0 RCM 2
1 44324U 19033C 25258.98946725 -.00000051 00000-0 41936-6 0 9991
2 44324 97.7603 265.4147 0001434 89.0748 271.0636 14.92588368341184Epoch: 2025-09-15T23:44Z
TLE epoch observation values (Epoch: 2025-09-15T23:44:49.97Z)
Latitude
0.00003°
Longitude
-85.97972°
Altitude
592.893 km
Speed
7.564 km/s
True Right ascension
17h 41m 39s
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
00:07:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.885 km
Perigee altitude
585.887 km
Semi-major axis
6,965.023 km
Eccentricity
0.00014
Inclination
97.7603°
RAAN
265.4147°
Arg. of periapsis
89.0748°
True anomaly
271.04717°
Mean anomaly
271.0636°
Eccentric anomaly
271.05539°
Mean motion
3.73387 °/min
Orbital period
96.41 mins
BSTAR
4.1936e-7
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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 | 2025-09-18 13:27:05.678Z | 10.4° NNE | 2025-09-18 13:30:05.678Z | 355.926° N | 42.871° | 2025-09-18 13:34:05.678Z | 196.471° SSW |
| 6 mins | 2025-09-19 00:17:05.678Z | 149.344° SSE | 2025-09-19 00:20:05.678Z | 63.931° ENE | 40.443° | 2025-09-19 00:23:05.678Z | 358.552° 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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