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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Edit Public Description
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, 20.4 m
Radar Cross Section
53.753 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 SPACEWAY 3
1 32018U 07036A 25296.56294847 .00000037 00000-0 00000+0 0 9998
2 32018 3.3854 79.9491 0003574 141.0202 221.8015 0.99141090 44119Epoch: 2025-10-23T13:30Z
TLE epoch observation values (Epoch: 2025-10-23T13:30:38.747Z)
Latitude
0.15873°
Longitude
-152.17839°
Altitude
36,117.429 km
Speed
3.062 km/s
True Right ascension
05h 30m 48s
True Declination
0° 09' 31"
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
02:00:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,122.82 km
Perigee altitude
36,092.451 km
Semi-major axis
42,485.773 km
Eccentricity
0.00036
Inclination
3.3854°
RAAN
79.9491°
Arg. of periapsis
141.0202°
True anomaly
221.77421°
Mean anomaly
221.8015°
Eccentric anomaly
221.78785°
Mean motion
0.24784 °/min
Orbital period
1,452.53 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 | 2025-10-24 06:49:06.513Z | 239.154° WSW | 2025-10-24 18:59:06.513Z | 246.1° WSW | 20.986° | 2025-10-25 06:49:06.513Z | 242.526° WSW |
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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
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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