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: 7 hours ago
TLE from 7 hours ago
0 TRANSIT 5E 3
1 00705U 63049C 25301.65898561 .00000128 00000-0 19286-3 0 9993
2 00705 89.9197 72.2558 0033305 198.3592 224.9012 13.47639305 40912Epoch: 2025-10-28T15:48Z
TLE epoch observation values (Epoch: 2025-10-28T15:48:56.356Z)
Latitude
63.07661°
Longitude
157.93499°
Altitude
1,109.522 km
Speed
7.295 km/s
True Right ascension
04h 49m 39s
True Declination
62° 56' 39"
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
17:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,102.843 km
Perigee altitude
1,053.177 km
Semi-major axis
7,456.147 km
Eccentricity
0.00333
Inclination
89.9197°
RAAN
72.2558°
Arg. of periapsis
198.3592°
True anomaly
224.63259°
Mean anomaly
224.9012°
Eccentric anomaly
224.76682°
Mean motion
3.3711 °/min
Orbital period
106.79 mins
BSTAR
0.00019286
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-29 07:41:16.435Z | 109.663° ESE | 2025-10-29 07:45:16.435Z | 71.808° E | 17.496° | 2025-10-29 07:49:16.435Z | 33.738° NE |
| 11 mins | 2025-10-29 09:26:16.435Z | 186.847° SSW | 2025-10-29 09:31:16.435Z | 274.952° WNW | 43.715° | 2025-10-29 09:37:16.435Z | 353.194° N |
| 11 mins | 2025-10-29 20:37:16.435Z | 15.951° NNE | 2025-10-29 20:42:16.435Z | 79.882° E | 37.856° | 2025-10-29 20:48:16.435Z | 161.289° S |
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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