WESTFORD NEEDLES, 18962
Orbit data source: Space-Track
WESTFORD NEEDLES, 18962 is space debris in LEO 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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18962 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: 19 hours ago
TLE from 19 hours ago
0 WESTFORD NEEDLES
1 18962U 63014DN 26235.16329027 .00001952 00000-0 29508+0 0 9998
2 18962 86.4679 142.9960 1411167 170.5508 192.5177 8.76733389208406Epoch: 2026-08-23T03:55Z
TLE epoch observation values (Epoch: 2026-08-23T03:55:08.279Z)
Latitude
0.00001°
Longitude
112.74821°
Altitude
4,935.352 km
Speed
5.51 km/s
True Right ascension
09h 31m 59s
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
14:01:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
4,955.999 km
Perigee altitude
2,152.717 km
Semi-major axis
9,932.495 km
Eccentricity
0.14112
Inclination
86.4679°
RAAN
142.996°
Arg. of periapsis
170.5508°
True anomaly
189.53132°
Mean anomaly
192.5177°
Eccentric anomaly
190.97798°
Mean motion
2.19258 °/min
Orbital period
164.19 mins
BSTAR
0.29508
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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. |
|---|---|---|---|---|---|---|---|
| 24 mins | 2026-08-24 05:25:49.766Z | 359.535° N | 2026-08-24 05:39:49.766Z | 92.346° ESE | 42.929° | 2026-08-24 05:49:49.766Z | 165.549° S |
| 15 mins | 2026-08-24 08:13:49.766Z | 335.89° NNW | 2026-08-24 08:21:49.766Z | 294.864° NW | 20.68° | 2026-08-24 08:28:49.766Z | 253.624° W |
| 31 mins | 2026-08-24 15:39:49.766Z | 113.58° SE | 2026-08-24 15:56:49.766Z | 66.55° ENE | 25.837° | 2026-08-24 16:10:49.766Z | 18° NNE |
| 44 mins | 2026-08-24 18:12:49.766Z | 178.054° S | 2026-08-24 18:38:49.766Z | 302.67° NW | 44.928° | 2026-08-24 18:56:49.766Z | 2.342° NNE |
| 32 mins | 2026-08-24 21:08:49.766Z | 247.651° W | 2026-08-24 21:25:49.766Z | 295.283° NW | 22.912° | 2026-08-24 21:40:49.766Z | 347.913° N |
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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