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: 4 hours ago
TLE from 4 hours ago
0 RCM 1
1 44322U 19033A 25261.15693846 .00001072 00000-0 10968-3 0 9996
2 44322 97.7604 267.5053 0001501 90.4632 269.6759 14.92584743341503Epoch: 2025-09-18T03:45Z
TLE epoch observation values (Epoch: 2025-09-18T03:45:59.482Z)
Latitude
-0.00007°
Longitude
-146.3151°
Altitude
592.928 km
Speed
7.563 km/s
True Right ascension
17h 50m 01s
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
00:10:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.943 km
Perigee altitude
585.852 km
Semi-major axis
6,965.034 km
Eccentricity
0.00015
Inclination
97.7604°
RAAN
267.5053°
Arg. of periapsis
90.4632°
True anomaly
269.6587°
Mean anomaly
269.6759°
Eccentric anomaly
269.6673°
Mean motion
3.73386 °/min
Orbital period
96.41 mins
BSTAR
0.00010968
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 12:24:15.776Z | 56.59° ENE | 2025-09-18 12:26:15.776Z | 88.472° E | 16.827° | 2025-09-18 12:29:15.776Z | 135.724° SSE |
| 5 mins | 2025-09-18 14:00:15.776Z | 335.852° NNW | 2025-09-18 14:02:15.776Z | 284.151° WNW | 29.543° | 2025-09-18 14:05:15.776Z | 227.436° WSW |
| 6 mins | 2025-09-19 00:49:15.776Z | 188.841° SSW | 2025-09-19 00:51:15.776Z | 238.521° WSW | 39.258° | 2025-09-19 00:55:15.776Z | 337.73° N |
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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