WESTFORD NEEDLES, 629
Orbit data source: Space-Track
WESTFORD NEEDLES, 629 is space debris in LEO originally from a launch on Thu, 09 May 1963 UTC via an ATLAS AGENA B launch vehicle from the Air Force Western Test Range (AFWTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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629 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
MIT-LL
Mission
Spacecraft
Bus & Motor
Unknown
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 WESTFORD NEEDLES
1 00629U 63014G 25294.74116995 -.00000042 00000-0 -21016-1 0 9994
2 00629 87.3462 213.9428 0056839 245.8936 113.5966 8.65565566973569Epoch: 2025-10-21T17:47Z
TLE epoch observation values (Epoch: 2025-10-21T17:47:17.083Z)
Latitude
-0.00002°
Longitude
-83.30316°
Altitude
3,667.14 km
Speed
6.293 km/s
True Right ascension
14h 15m 46s
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
04:41:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,696.645 km
Perigee altitude
3,582.764 km
Semi-major axis
10,017.841 km
Eccentricity
0.00568
Inclination
87.3462°
RAAN
213.9428°
Arg. of periapsis
245.8936°
True anomaly
114.19176°
Mean anomaly
113.5966°
Eccentric anomaly
113.89435°
Mean motion
2.16462 °/min
Orbital period
166.31 mins
BSTAR
-0.021016
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Other satellites on launch #14 in the year 1963 (1963-05-09 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.WESTFORD NEEDLES 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. |
|---|---|---|---|---|---|---|---|
| 22 mins | 2025-10-22 16:11:16.795Z | 93.983° ESE | 2025-10-22 16:22:16.795Z | 55.63° ENE | 19.402° | 2025-10-22 16:33:16.795Z | 18.308° NNE |
| 36 mins | 2025-10-22 18:46:16.795Z | 170.047° S | 2025-10-22 19:03:16.795Z | 103.541° ESE | 44.697° | 2025-10-22 19:22:16.795Z | 3.219° NNE |
| 29 mins | 2025-10-22 21:39:16.795Z | 244.635° WSW | 2025-10-22 21:53:16.795Z | 296.776° NW | 24.86° | 2025-10-22 22:08:16.795Z | 350.937° N |
| 25 mins | 2025-10-23 03:53:16.795Z | 15.155° NNE | 2025-10-23 04:05:16.795Z | 58.491° ENE | 21.195° | 2025-10-23 04:18:16.795Z | 105.537° ESE |
| 36 mins | 2025-10-23 06:38:16.795Z | 358.302° N | 2025-10-23 06:56:16.795Z | 137.337° SSE | 44.978° | 2025-10-23 07:14:16.795Z | 182.564° SSW |
| 10 mins | 2025-10-23 09:27:16.795Z | 340.536° N | 2025-10-23 09:37:16.795Z | 305.159° NW | 22.531° | 2025-10-23 09:37:16.795Z | 305.159° NW |
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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