RCM 1, 44322
Orbit data source: Space-Track
RCM 1, 44322 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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44322 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: 6 hours ago
TLE from 6 hours ago
0 RCM 1
1 44322U 19033A 25318.00608639 -.00000244 00000-0 -18353-4 0 9998
2 44322 97.7597 323.5365 0001497 90.7949 269.3441 14.92592664349987Epoch: 2025-11-14T00:08Z
TLE epoch observation values (Epoch: 2025-11-14T00:08:45.864Z)
Latitude
-0.00007°
Longitude
-92.01037°
Altitude
592.91 km
Speed
7.563 km/s
True Right ascension
21h 34m 08s
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
03:01:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.915 km
Perigee altitude
585.83 km
Semi-major axis
6,965.01 km
Eccentricity
0.00015
Inclination
97.7597°
RAAN
323.5365°
Arg. of periapsis
90.7949°
True anomaly
269.32695°
Mean anomaly
269.3441°
Eccentric anomaly
269.33552°
Mean motion
3.73388 °/min
Orbital period
96.41 mins
BSTAR
-0.000018353
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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 1 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 13:34:40.525Z | 5.709° NNE | 2025-11-14 13:38:40.525Z | 252.045° W | 41.654° | 2025-11-14 13:41:40.525Z | 204.405° SW |
| 7 mins | 2025-11-15 00:24:40.525Z | 158.465° S | 2025-11-15 00:27:40.525Z | 77.169° E | 43.856° | 2025-11-15 00:31:40.525Z | 351.696° 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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