TRANSIT 5E 3, 705
Orbit data source: Space-Track
TRANSIT 5E 3, 705 is a payload satellite owned by USN BuWeps (US) in LEO that was launched on Thu, 05 Dec 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
52 kg wet, 52 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 TRANSIT 5E 3
1 00705U 63049C 25315.31857549 .00000140 00000-0 21221-3 0 9998
2 00705 89.9216 72.1475 0034585 159.2757 254.2524 13.47642238 42758Epoch: 2025-11-11T07:38Z
TLE epoch observation values (Epoch: 2025-11-11T07:38:44.922Z)
Latitude
53.24104°
Longitude
-93.1421°
Altitude
1,096.806 km
Speed
7.305 km/s
True Right ascension
04h 49m 00s
True Declination
53° 05' 01"
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
05:26:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,103.786 km
Perigee altitude
1,052.212 km
Semi-major axis
7,456.136 km
Eccentricity
0.00346
Inclination
89.9216°
RAAN
72.1475°
Arg. of periapsis
159.2757°
True anomaly
253.87141°
Mean anomaly
254.2524°
Eccentric anomaly
254.06186°
Mean motion
3.37111 °/min
Orbital period
106.79 mins
BSTAR
0.00021221
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Other satellites on launch #49 in the year 1963 (1963-12-05 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 5E 3 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-12 19:38:05.824Z | 19.81° NNE | 2025-11-12 19:43:05.824Z | 94.588° ESE | 36.192° | 2025-11-12 19:48:05.824Z | 156.818° SSE |
| 9 mins | 2025-11-12 21:25:05.824Z | 330.849° NNW | 2025-11-12 21:29:05.824Z | 285.025° WNW | 24.233° | 2025-11-12 21:34:05.824Z | 232.032° WSW |
| 11 mins | 2025-11-13 07:37:05.824Z | 146.871° SSE | 2025-11-13 07:42:05.824Z | 72.542° E | 36.676° | 2025-11-13 07:48:05.824Z | 9.502° NNE |
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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