TRANSIT 5B-1, 670
Orbit data source: Space-Track
TRANSIT 5B-1, 670 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Sat, 28 Sep 1963 UTC via a THOR ABLESTAR 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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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
69 kg wet, 69 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TRANSIT 5B-1
1 00670U 63038B 25315.04877742 .00000106 00000-0 16529-3 0 9991
2 00670 89.9694 333.6095 0039820 300.3642 59.3572 13.44643615 44870Epoch: 2025-11-11T01:10Z
TLE epoch observation values (Epoch: 2025-11-11T01:10:14.369Z)
Latitude
0.00009°
Longitude
-94.39129°
Altitude
1,079.901 km
Speed
7.319 km/s
True Right ascension
22h 14m 26s
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
01:35:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,118.823 km
Perigee altitude
1,059.354 km
Semi-major axis
7,467.226 km
Eccentricity
0.00398
Inclination
89.9694°
RAAN
333.6095°
Arg. of periapsis
300.3642°
True anomaly
59.75078°
Mean anomaly
59.3572°
Eccentric anomaly
59.55389°
Mean motion
3.3636 °/min
Orbital period
107.03 mins
BSTAR
0.00016529
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Other satellites on launch #38 in the year 1963 (1963-09-28 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.TRANSIT 5B-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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-12 13:29:43.106Z | 7.231° NNE | 2025-11-12 13:34:43.106Z | 56.025° ENE | 43.539° | 2025-11-12 13:41:43.106Z | 176.574° S |
| 6 mins | 2025-11-12 15:18:43.106Z | 314.901° NW | 2025-11-12 15:21:43.106Z | 284.221° WNW | 17.187° | 2025-11-12 15:24:43.106Z | 255.683° W |
| 12 mins | 2025-11-13 01:29:43.106Z | 168.776° S | 2025-11-13 01:35:43.106Z | 48.712° ENE | 43.889° | 2025-11-13 01:41:43.106Z | 1.181° NNE |
| 6 mins | 2025-11-13 03:20:43.106Z | 260.965° W | 2025-11-13 03:22:43.106Z | 281.109° WNW | 15.978° | 2025-11-13 03:26:43.106Z | 318.75° NNW |
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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