WESTFORD NEEDLES, 2367
Orbit data source: Space-Track
WESTFORD NEEDLES, 2367 is space debris originally from a launch on Thu, 09 May 1963 UTC launched 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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2367 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 WESTFORD NEEDLES
1 2367U 63014S 26167.09566691 .00063705 00000-0 44399-1 0 9997
2 2367 84.2469 59.5568 2908184 102.8657 290.8987 9.06884775 11898Epoch: 2026-06-16T02:17Z
TLE epoch observation values (Epoch: 2026-06-16T02:17:45.621Z)
Latitude
-0.00002°
Longitude
120.74409°
Altitude
3,126.85 km
Speed
6.547 km/s
True Right ascension
03h 58m 13s
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
20:44:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,156.746 km
Perigee altitude
508.586 km
Semi-major axis
9,710.803 km
Eccentricity
0.29082
Inclination
84.2469°
RAAN
59.5568°
Arg. of periapsis
102.8657°
True anomaly
257.23567°
Mean anomaly
290.8987°
Eccentric anomaly
274.28256°
Mean motion
2.26809 °/min
Orbital period
158.72 mins
BSTAR
0.044399
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-16 15:38:59.925Z | 126.382° SE | 2026-06-16 15:44:59.925Z | 93.368° ESE | 17.637° | 2026-06-16 15:48:59.925Z | 57.157° ENE |
| 16 mins | 2026-06-16 18:13:59.925Z | 203.751° SW | 2026-06-16 18:24:59.925Z | 268.994° W | 36.101° | 2026-06-16 18:29:59.925Z | 343.173° N |
| 9 mins | 2026-06-17 05:22:59.925Z | 327.954° NNW | 2026-06-17 05:24:59.925Z | 279.754° WNW | 37.039° | 2026-06-17 05:31:59.925Z | 193.138° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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