SPACEWAY 3, 32018
Orbit data source: Space-Track
SPACEWAY 3, 32018 is a payload satellite owned by Hughes NS (US) in GEO that was launched on Tue, 14 Aug 2007 UTC via an ARIANE 5ECA launch vehicle from the French Guiana (FRGUI). 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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32018 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/ES
Mission
Non-operational Commercial Communications
Bus & Motor
BSS-702HP, R-4D-15-375
Mass
6,075 kg wet, 3,655 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 20.5 m
Radar Cross Section
53.753 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 SPACEWAY 3
1 32018U 07036A 26263.49781584 -.00000164 00000-0 00000-0 0 9997
2 32018 4.2431 75.9426 0001420 138.5343 259.7745 0.99139974 47402Epoch: 2026-09-20T11:56Z
TLE epoch observation values (Epoch: 2026-09-20T11:56:51.288Z)
Latitude
2.61215°
Longitude
-64.46344°
Altitude
36,107.151 km
Speed
3.063 km/s
True Right ascension
07h 36m 33s
True Declination
2° 36' 34"
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
00:08:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,113.985 km
Perigee altitude
36,101.919 km
Semi-major axis
42,486.089 km
Eccentricity
0.00014
Inclination
4.2431°
RAAN
75.9426°
Arg. of periapsis
138.5343°
True anomaly
259.75849°
Mean anomaly
259.7745°
Eccentric anomaly
259.76649°
Mean motion
0.24784 °/min
Orbital period
1,452.54 mins
BSTAR
0
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Other satellites on launch #36 in the year 2007 (2007-08-14 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.SPACEWAY 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. |
|---|---|---|---|---|---|---|---|
| 1440 mins | 2026-09-21 07:07:55.199Z | 131.644° SE | 2026-09-21 16:01:55.199Z | 128.187° SE | 34.705° | 2026-09-22 07:07:55.199Z | 135.984° SSE |
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32018 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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